an experimental investigation of impingement heat …1693/...iv figure 24. nusselt number versus...

251
An Experimental Investigation of Impingement Heat Transfer in a Rib-Roughened Trailing-Edge Channel with Crossover Holes A thesis presented by Xiao Huang to The Department of Mechanical and Industrial Engineering in partial fulfillment of the requirements for the degree of Master of Science in Mechanical Engineering In the field of Thermofluids Engineering Northeastern University Boston Massachusetts August 2012

Upload: doancong

Post on 25-Jun-2018

213 views

Category:

Documents


0 download

TRANSCRIPT

i

An Experimental Investigation of Impingement Heat Transfer in a Rib-Roughened

Trailing-Edge Channel with Crossover Holes

A thesis presented

by

Xiao Huang

to

The Department of Mechanical and Industrial Engineering

in partial fulfillment of the requirements for the degree of

Master of Science

in

Mechanical Engineering

In the field of

Thermofluids Engineering

Northeastern University

Boston Massachusetts

August 2012

i

Abstract

Turbine cooling technology plays a critical role in increasing the thermal efficiency and

power output of advanced gas turbines. The common cooling methods include the

impingement cooling method, the film cooling method, and the rib roughened cooling

method. This study focuses on the impingement cooling effect on a rib-roughened trailing

edge channel with cross over holes and aims to find the influence of blocked exit holes to

the heat transfer efficiency.

A steady state liquid crystal technique was used to get the heat transfer coefficient. In this

experiment, two different kinds of cross-over holes were used: five tilt angle and zero tilt

angle. Both inline and staggered slot-arrangement were tested and investigated. There

were total 16 geometry cases. The numbers of blocked exit holes are 0, 3, 4 and 5 for

inline arrangement and 0, 2, 3 and 4 for staggered arrangement. For each geometry

setting, a range of Reynolds numbers was tested. The graphs of the Nusselt number

versus the Reynolds number were plotted. For each individual area, the Nusselt numbers

with different number of blocked exit holes were compared. The results showed that the

Nusselt numbers increase monotonically with increasing Reynolds numbers. It was also

found that for staggered arrangement, the highest Nusselt numbers were found in the area

two holes away from the nearest blocked exit hole. And for inline arrangement,

conclusions are different between zero tilt angle and five tilt angle. With zero tilt angle,

the Nusselt numbers of area1 and area2 both increased first and then decreased as the

number of blocked holes increased. While with five tilt angle, Nusselt numbers of all the

four areas decreased monotonically.

ii

Table of Contents

Introduction……………………………………………………………………………………...…..

Experimental set up and procedure……………………………………………………………...…..

Experimental set up……………………………………………………………………………….

Experimental procedure…………………………………………………………………………..

Liquid crystal calibration………………………………………………………………………

Cold and heat transfer tests…………………………………………………………………….

Date reduction……………………………………………………………………………………….

Results and discussion………………………………………………………………………………

Conclusion………………………………………………………………………… ………………..

References………………………………………………………………………… ...………….......

Appendix A: Log sheets for each experiment…………………………………….. .………………

Appendix B: Source code for 𝐶𝑕𝑒𝑐𝑘.𝑓………………………………………………………..........

Appendix C: Source code for 𝑅𝑒𝑑𝑢𝑐𝑒. 𝑓……………………………………………………………

Appendix D: Source code for 𝑖𝑛𝑡𝑒𝑟𝑔𝑎𝑟𝑒𝑎.𝑓…………………………………………………........

1

4

4

14

14

15

27

38

97

99

A-1

B-1

C-1

D-1

iii

List of Figures

Figure 1. Gas turbine engine………………………………………………………………….

Figure 2. Idealized Brayton Cycle……………………………………………….…….……..

Figure 3. The common cooling techniques for a modern gas turbine blade……..…………..

Figure 4. Schematics of the test section…………………………………………..………….

Figure 5. cross section of the supply channel and trailing edge channel togther…..………...

Figure 6. The locations of the pressure taps………………………………………..………...

Figure 7. Details of the cross-over holes (removable partition holes)………………...……...

Figure 8. Details of the trailing edge channel…………………………………………..……

Figure 9. Details of the trailing edge holes………………………………………………..…

Figure 10. The dimensions of the turbulators used in experiment…………………………...

Figure 11. Inline arrangement flow………………………………………………………….

Figure 12. Staggered arrangement flow……………………………………………………...

Figure 13. Camera focuses and the four areas for staggered arrangement…………………..

Figure 14. Camera focuses and the four areas for inline arrangement……………………....

Figure 15. Liquid crystal display of the reference color and the reference temperature…….

Figure 16. Thermometer used in experiment………………………………………………..

Figure 17. True-rms Multimeter used in experiment………………………………………..

Figure 18. Micro-manometer used in experiment……………………………………………

Figure 19. Orange-manometer used in experiment………………………………………….

Figure 20. Red-manometer used in experiment……………………………………………..

Figure 21. Electrical power panel used in experiment………………………………….……

Figure 22. Nusselt Number versus Reynolds Number for geometry 1 (11crossover holes-12

exit holes, inline arrangement, 0 degree tilt angle case) at different pressure

increments…………………………………………………………………….….

Figure 23. Nusselt Number versus Reynolds Number for geometry 2 (11crossover holes-9

exit holes, inline arrangement, 0 degree tilt angle case) at different pressure

increments………………………………………………………………….……..

1

2

3

4

6

7

8

9

9

10

11

12

13

13

15

21

21

23

23

24

24

40

41

iv

Figure 24. Nusselt Number versus Reynolds Number for geometry 3 (11crossover holes-8

exit holes, inline arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….41

Figure 25. Nusselt Number versus Reynolds Number for geometry 4 (11crossover holes-7

exit holes, inline arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….42

Figure 26. Nusselt Number versus Reynolds Number for geometry 5 (11crossover holes-12

exit holes, inline arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….42

Figure 27. Nusselt Number versus Reynolds Number for geometry 6 (11crossover holes-9

exit holes, inline arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….43

Figure 28. Nusselt Number versus Reynolds Number for geometry 7 (11crossover holes-8

exit holes, inline arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….43

Figure 29. Nusselt Number versus Reynolds Number for geometry 8 (11crossover holes-7

exit holes, inline arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….44

Figure 30. Nusselt Number versus Reynolds Number for geometry 9 (11crossover holes-12

exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….44

Figure 31. Nusselt Number versus Reynolds Number for geometry 10 (11crossover holes-10

exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….45

Figure 32. Nusselt Number versus Reynolds Number for geometry 11(11crossover holes-9

exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….45

Figure 33. Nusselt Number versus Reynolds Number for geometry 12(11crossover holes-8

exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments……………………………………………………………………….46

Figure 34. Nusselt Number versus Reynolds Number for geometry 13 (11crossover holes-12

exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….46

Figure 35. Nusselt Number versus Reynolds Number for geometry 14 (11crossover holes-

10 exit holes, staggered arrangement, 5 degree tilt angle case) at different

pressure increments……………………………………………………………...47

Figure 36. Nusselt Number versus Reynolds Number for geometry 15 (11crossover holes-9

exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….47

v

Figure 37. Nusselt Number versus Reynolds Number for geometry 16(11crossover holes-8

exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments……………………………………………………………………….48

Figure 38. Nusselt Number versus Reynolds Number of four areas for geometry 1

(11crossover holes-12 exit holes, inline arrangement, 0 degree tilt angle)

case………………………………………………………………………………48

Figure 39. Nusselt Number versus Reynolds Number of four areas for geometry 2

(11crossover holes-9 exit holes, inline arrangement, 0 degree tilt angle)

case………………………………………………………………………………49

Figure 40. Nusselt Number versus Reynolds Number of four areas for geometry 3

(11crossover holes-8 exit holes, inline arrangement, 0 degree tilt angle)

case………………………………………………………………………………49

Figure 41. Nusselt Number versus Reynolds Number of four areas for geometry 4

(11crossover holes-7 exit holes, inine arrangement, 0 degree tilt angle)

case………………………………………………………………………………50

Figure 42. Nusselt Number versus Reynolds Number of four areas for geometry 5

(11crossover holes-12 exit holes, inline arrangement, 5 degree tilt angle)

case………………………………………………………………………………50

Figure 43. Nusselt Number versus Reynolds Number of four areas for geometry 6

(11crossover holes-9 exit holes, inline arrangement, 5 degree tilt angle)

case………………………………………………………………………………51

Figure 44. Nusselt Number versus Reynolds Number of four areas for geometry 7

(11crossover holes-8 exit holes, inline arrangement, 5 degree tilt angle)

case………………………………………………………………………………51

Figure 45. Nusselt Number versus Reynolds Number of four areas for geometry 8

(11crossover holes-7 exit holes, inline arrangement, 5 degree tilt angle)

case………………………………………………………………………………52

Figure 46. Nusselt Number versus Reynolds Number of four areas for geometry 9

(11crossover holes-12 exit holes, staggered arrangement, 0 degree tilt angle)

case………………………………………………………………………………52

Figure 47. Nusselt Number versus Reynolds Number of four areas for geometry 10

(11crossover holes-10 exit holes, staggered arrangement, 0 degree tilt angle)

case………………………………………………………………………………53

Figure 48. Nusselt Number versus Reynolds Number of four areas for geometry 11

(11crossover holes-9 exit holes, staggered arrangement, 0 degree tilt angle)

case………………………………………………………………………………53

Figure 49. Nusselt Number versus Reynolds Number of four areas for geometry 12

(11crossover holes-8 exit holes, staggered arrangement, 0 degree tilt angle)

case………………………………………………………………………………54

vi

Figure 50. Nusselt Number versus Reynolds Number of four areas for geometry 13

(11crossover holes-12 exit holes, staggered arrangement, 5 degree tilt angle)

case………………………………………………………………………………54

Figure 51. Nusselt Number versus Reynolds Number of four areas for geometry 14

(11crossover holes-10 exit holes, staggered arrangement, 5 degree tilt angle)

case………………………………………………………………………………55

Figure 52. Nusselt Number versus Reynolds Number of four areas for geometry 15

(11crossover holes-9 exit holes, staggered arrangement, 5 degree tilt angle)

case………………………………………………………………………………55

Figure 53. Nusselt Number versus Reynolds Number of four areas for geometry 16

(11crossover holes-8 exit holes, staggered arrangement, 5 degree tilt angle)

case………………………………………………………………………………56

Figure 54. Nusselt Number versus Reynolds Number for geometry 1 (11crossover holes-12

exit holes, inline arrangement, 0 degree tilt angle) case………………………...56

Figure 55. Nusselt Number versus Reynolds Number for geometry 2 (11crossover holes-9

exit holes, inline arrangement, 0 degree tilt angle) case………………………...57

Figure 56. Nusselt Number versus Reynolds Number for geometry 3 (11crossover holes-8

exit holes, inline arrangement, 0 degree tilt angle) case………………………...57

Figure 57. Nusselt Number versus Reynolds Number for geometry 4 (11crossover holes-7

exit holes, inline arrangement, 0 degree tilt angle) case………………………...58

Figure 58. Nusselt Number versus Reynolds Number for geometry 5 (11crossover holes-12

exit holes, inline arrangement, 5 degree tilt angle) case………………………...58

Figure 59. Nusselt Number versus Reynolds Number for geometry 6 (11crossover holes-9

exit holes, inline arrangement, 5 degree tilt angle) case………………………...59

Figure 60. Nusselt Number versus Reynolds Number for geometry 7 (11crossover holes-8

exit holes, inline arrangement, 5 degree tilt angle) case………………………...59

Figure 61. Nusselt Number versus Reynolds Number for geometry 8 (11crossover holes-7

exit holes, inline arrangement, 5 degree tilt angle) case………………………...60

Figure 62. Nusselt Number versus Reynolds Number for geometry 9 (11crossover holes-12

exit holes, staggered arrangement, 0 degree tilt angle) case…………………….60

Figure 63. Nusselt Number versus Reynolds Number for geometry 10 (11crossover holes-

10 exit holes, staggered arrangement, 0 degree tilt angle) case…………………61

Figure 64. Nusselt Number versus Reynolds Number for geometry 11 (11crossover holes-9

exit holes, staggered arrangement, 0 degree tilt angle) case…………………….61

Figure 65. Nusselt Number versus Reynolds Number for geometry 12 (11crossover holes-8

exit holes, staggered arrangement, 0 degree tilt angle) case…………………….62

vii

Figure 66. Nusselt Number versus Reynolds Number for geometry 13 (11crossover holes-12

exit holes, staggered arrangement, 5 degree tilt angle) case…………………….62

Figure 67. Nusselt Number versus Reynolds Number for geometry 14 (11crossover holes-10

exit holes, staggered arrangement, 5 degree tilt angle) case…………………….63

Figure 68. Nusselt Number versus Reynolds Number for geometry 15 (11crossover holes-9

exit holes, staggered arrangement, 5 degree tilt angle) case…………………….63

Figure 69. Nusselt Number versus Reynolds Number for geometry 16 (11crossover holes-8

exit holes, staggered arrangement, 5 degree tilt angle) case…………………….64

Figure 70. Nusselt Number versus Reynolds Number for Area 1 at different number of exit

holes cases (inline arrangement, zero degree tilt angle)………………………...64

Figure 71. Nusselt Number versus Reynolds Number for Area 2 at different number of exit

holes cases (inline arrangement, zero degree tilt angle)………………………...65

Figure 72. Nusselt Number versus Reynolds Number for Area 3 at different number of exit

holes cases (inline arrangement, zero degree tilt angle)………………………...65

Figure 73. Nusselt Number versus Reynolds Number for Area 3 at different number of exit

holes cases (inline arrangement, zero degree tilt angle)………………………...66

Figure 74. Nusselt Number versus Reynolds Number for Area 1 at different number of exit

holes cases (inline arrangement, five degree tilt angle)…………………………66

Figure 75. Nusselt Number versus Reynolds Number for Area 2 at different number of exit

holes cases (inline arrangement, five degree tilt angle)…………………………67

Figure 76. Nusselt Number versus Reynolds Number for Area 3 at different number of exit

holes cases (inline arrangement, five degree tilt angle)…………………………67

Figure 77. Nusselt Number versus Reynolds Number for Area 4 at different number of exit

holes cases (inline arrangement, five degree tilt angle)…………………………68

Figure 78. Nusselt Number versus Reynolds Number for Area 1 at different number of exit

holes cases (staggered arrangement, zero degree tilt angle)…………………….68

Figure 79. Nusselt Number versus Reynolds Number for Area 2 at different number of exit

holes cases (staggered arrangement, zero degree tilt angle)…………………….69

Figure 80. Nusselt Number versus Reynolds Number for Area 3 at different number of exit

holes cases (staggered arrangement, zero degree tilt angle)…………………….69

Figure 81. Nusselt Number versus Reynolds Number for Area 4 at different number of exit

holes cases (staggered arrangement, zero degree tilt angle)…………………….70

Figure 82. Nusselt Number versus Reynolds Number for Area 1 at different number of exit

holes cases (staggered arrangement, five degree tilt angle)……………………..70

Figure 83. Nusselt Number versus Reynolds Number for Area 2 at different number of exit

holes cases (staggered arrangement, five degree tilt angle)……………………..71

viii

Figure 84. Nusselt Number versus Reynolds Number for Area 3 at different number of exit

holes cases (staggered arrangement, five degree tilt angle)……………………..71

Figure 85. Nusselt Number versus Reynolds Number for Area 4 at different number of exit

holes cases (staggered arrangement, five degree tilt angle)……………………..72

Figure 86. Nu Vs Re (Area 1 for different arrangement of 11crossover holes-12exit

holes)…………………………………………………………………………….72

Figure 87. Nu Vs Re (Area 2 for different arrangement of 11crossover holes-12exit

holes)…………………………………………………………………………….73

Figure 88. Nu Vs Re (Area 3 for different arrangement of 11crossover holes-12exit

holes)…………………………………………………………………………….73

Figure 89. Nu Vs Re (Area 4 for different arrangement of 11crossover holes-12exit

holes)…………………………………………………………………………….74

Figure 90. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-10exit

holes)…………………………………………………………………………….74

Figure 91. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-10exit

holes)…………………………………………………………………………….75

Figure 92. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-10exit

holes)…………………...………………………………………………………..75

Figure 93. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-10exit

holes)……………………………………………………………………………76

Figure 94. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-9exit

holes)……………..……………………………………………………………..76

Figure 95. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-9exit

holes)…………………..………………………………………………………...77

Figure 96. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-9exit

holes)………………………………………………………………………….....77

Figure 97. Nu Vs Re (Area 4 for inline arrangement 11crossover holes-9exit

holes)……………..…….......................................................................................78

Figure 98. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-9exit

holes)…………………….………………………………………………………78

Figure 99. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-9exit

holes)…………………….………………………………………………………79

Figure 100. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-9exit

holes)………………...…………………………………………………………..79

Figure 101. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-9exit

holes)……………….……………………………………………………………80

ix

Figure 102. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-8exit

holes)…………………………………………………………………………….80

Figure 103. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-8exit

holes)……………….……………………………………………………………81

Figure 104. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-8exit

holes)…………………………………………………………………………….81

Figure 105. Nu Vs Re (Area 4 for inline arrangement 11crossover-8exit

holes)……………………………….……………………………………………82

Figure 106. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-8exit

holes)…………………………………………………………………………….82

Figure 107. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-8exit

holes)……………….……………………………………………………………83

Figure 108. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-8exit

holes)…………………………………………………………………………….83

Figure 109. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-8exit

holes)………………………….…………………………………………………84

Figure 110. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-7exit

holes)………...…………………………………………………………………..84

Figure 111. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-7exit

holes)…………………….………………………………………………………85

Figure 112. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-7exit

holes)………………….…………………………………………………………85

Figure 113. Nu Vs Re (Area 4 for inline arrangement 11crossover holes-7exit

holes)……….……………………………………………………………………86

x

Nomenclature

𝑚 Air mass flow rate entering the test section

𝐴𝑣𝑒𝑛 Throat area of the critical venturi

𝑃𝑎𝑚𝑏 Ambient pressure

𝑃𝑣𝑒𝑛 Air pressure at the inlet of the critical venture (gage)

𝑇𝑣𝑒𝑛 Air temperature at the inlet of the critical venturi

𝑅𝑒𝑗𝑒𝑡 Reynolds Number based on the cross-over hole hydraulic diameter

𝜇𝑗𝑒𝑡 Air dynamic viscosity at the jet temperature

𝑚𝑏𝑙𝑒𝑒𝑑 Air mass flow rate from the bleed hole

𝐴𝑏𝑙𝑒𝑒𝑑 Total bleed area

𝐴𝑐𝑟𝑜𝑠𝑠 Supply channel cross sectional area

𝑄 Total heat added to the air by the surface heaters

𝑉 Voltage across the heater

𝐴 Amperage through the heater

𝑄" Heat flux at the Liquid crystal wall

𝑇𝐹 Film temperature

xi

𝑇𝑏𝑎𝑐𝑘 Temperature of the back wall

𝑇𝑚 Air mixed mean temperature

𝑁𝑢𝑗𝑒𝑡 Nusselt number based on the cross-over hole hydraulic diameter

𝑕𝑡𝑢𝑟𝑏 Heat transfer coefficient on the turbulated target wall

𝐷𝑕 Cooling channel hydraulic diameter

𝐾 Air thermal conductivity

𝑕0 Outer natural convection heat transfer coefficient

𝐾𝑎𝑚𝑏 Air thermal conductivity at ambient temperature

𝐷𝑒 Hydraulic diameter of the outside of test

𝑇𝑕𝑒𝑎𝑡𝑒𝑟 Channel heater temperature

𝑇𝑙𝑖𝑞𝑢𝑖𝑑 Reference temperature of the liquid crystal

𝑇𝑎𝑚𝑏𝑖𝑒𝑛𝑡 Ambient temperature

𝑅𝑏𝑎𝑐𝑘 Thermal resistance of the back wall

𝑅𝑓𝑟𝑜𝑛𝑡 Thermal resistance from the heating element center to the air inside

the test section

𝑅1 Thermal resistance for the front wall

𝑅𝑡𝑜𝑝 Thermal resistance for the top wall

xii

𝑅𝑏𝑜𝑡 Thermal resistance for the bottom wall

𝐹𝑙𝑢𝑥𝑡𝑜𝑝 Heat flux from top wall

𝐹𝑙𝑢𝑥𝑓 Heat flux from front wall

𝐹𝑙𝑢𝑥𝑏𝑜𝑡 Heat flux from bottom wall

𝐹𝑙𝑢𝑥𝑏 Heat flux from back wall

𝐹𝑙𝑏𝑎𝑐𝑘 Heat loss from back wall

𝐹𝑓𝑟𝑜𝑛𝑡 Heat loss for front side inside the section

𝐻𝑒𝑎𝑡𝑝𝑒𝑟𝑙𝑜𝑠𝑠 The percentage of heat loss

𝐹𝑙𝑡𝑜𝑝 Heat loss from top wall

𝐹𝑙𝑏𝑜𝑡 Heat loss from bottom wall

𝑄𝑤𝑎𝑠𝑡𝑒𝑑 The total heat loss to the ambient air via radiation and conduction

𝑄𝑎𝑑𝑑 The net heat added to the from the inlet to the point in question

xiii

Acknowledgements

I would send out my greatest thanks to Professor Mohammed Taslim whose

encouragement, guidance and support enabled me to finish this thesis. I want to thank

Professor Mohammed Taslim for introducing me to his research.

My deep sense of gratitude is to Sultan Al shehery, Nathaniel Risler Rosso, Mian

Cao and Mehdi Abedi for their help and guidance throughout this work.

1

Introduction

Gas turbines are now widely used for aircraft propulsion, land-based power generation,

and industrial applications. Gas turbine converts the fuel energy into practical power. Jet

engine is one kind of the gas turbines. Figure1 shows the structure of one kind of jet

engine and its working principle.

Figure 1. Gas turbine engine

In the jet engine, air is first compressed to high pressure and temperature, then mixed and

burned with fuel in the combustion chamber. The hot exhaust gases then turn the turbine

which drive the compressor, and provide forward thrust.

2

The basic thermodynamic cycle for gas turbine is known as Brayton cycle. It is shown in

Figure 2.

Figure 2. Idealized Brayton Cycle

To improve thermal efficiency and power output of the gas turbine, high turbine inlet

temperature is needed. Advanced gas turbine engines operate at high temperatures around

1200-1500℃. However, as the turbine inlet temperature increases, the heat transfer to the

turbine blade also increases which raises another issue, that is, the turbine blades’ life

gets shorten. The level and variation in the temperature within the blade material, which

cause thermal stresses, must be limited to achieve reasonable durability goals. The

operating temperatures exceed the melting point temperatures of the turbine blade

materials. Therefore, turbine cooling technology plays a critical role in increasing the

thermal efficiency and power output of advanced gas turbines.

Figure 3 shows the common cooling technology with three major internal cooling zones

in a turbine blade.

3

Figure 3. The common cooling techniques for a modern gas turbine blade

The leading edge is cooled by jet impingement with film cooling, the middle portion is

cooled by serpentine rib-roughened passages with local film cooling, and the trailing

edge is cooled by pin fins with trailing edge injection.

This experiment focuses on the impingement cooling effect on a rib-roughened trailing

edge channel with cross over holes and aims to find the influence of blocked exit holes to

the heat transfer efficiency.

4

Experimental set up and Procedure

Experimental set up

To model the coolant flow in a typical gas turbine airfoil, we use a laboratory setting

which is shown in Figure 4.

Figure 4. Schematics of the test section

This set up is made out of clear acrylic plastic, and has to endure the process of being

taken apart, adjusted, put back together, and sealed again.

In this experiment, the moving air is used to represent the coolant flowing in a real

turbine airfoil. A compressor stores air in a reservoir, which is then dispensed into the

pipe system through which air is sent to the laboratory room. Then the air travels through

a heat exchanger system, the critical venture, and finally into the experiment setup.

5

The temperature of the inlet air plays a crucial role in this experiment. Lower inlet air

temperature gives lower uncertainty of the test results which means that the results are

more accurate. So before the air travels into the test section, a heat exchanger system is

used to cool it down, especially when the atmospheric air temperature is high outside the

laboratory. The reason is because of the size of the reservoir, it is emptied within an hour,

whereas a typical experiment takes up to 5 hours. When the reservoir is emptied, the air

comes directly from the compressor at a somehow higher temperature due to the hot

weather outside. By using the heat exchanger, air is cooled at an appropriate temperature

to make sure the results are acceptable. The heat exchanger system has an inner and outer

diameter of 2.5” and 4”, respectively.

The critical venturi has a throat of diameter of 0.32 inches, and is used for measuring the

total mass flow rate. A thermal couple and a pressure tap are attached to the critical

venturi to get the temperature 𝑇𝑣𝑒𝑛 and pressure 𝑃𝑣𝑒𝑛 of the air inside.

Finally air at specific pressure and low temperature travels to the test section which is

shown in Figure4. The test section can be taken apart into three parts, which are the

plenum, the supply channel and the trailing edge channel. First, air goes in the plenum

and gets filtered. Then clean and dried air enters the supply channel and exits from the

trailing edge channel.

The plenum has a cubical shape of 20" × 20" × 20" with a wall thickness of 1”. A

honeycomb flow straightener is placed in a groove in the middle of the plenum. Two

thermocouples and a pressure tap are placed on the plenum to measure the inlet air

temperature Tin 1, Tin 2 and the plenum pressurePplen , which can be found in figure 4.

6

Figure 5 below shows the cross-section of the supply channel and the trailing edge

channel.

Figure 5. cross section of the supply channel and trailing edge channel togther

The supply channel has a trapezoidal cross-section with a length of 49 inches, and is

made of 0.5 inches thick acrylic plastic. The front, back and bottom walls of the supply

channel are all rectangular. On the top, there is a removable partition wall which has 11

cross-over holes on it. Cooling air comes in from left side, travels through the cross-over

holes on the top then enters in the trailing edge channel. In the middle of the bottom wall

of the supply channel, a thermocouple is mounted to measure the jet temperature 𝑇𝑗𝑒𝑡 .

Two pressure taps are placed on the front wall to measure the pressures in the supply

channel 𝑃𝑠𝑢𝑝1 𝑎𝑛𝑑 𝑃𝑠𝑢𝑝2 . 𝑃𝑠𝑢𝑝1 locates 17 inches away from the plenum, and 𝑃𝑠𝑢𝑝2 tap

is 13.25 inches away from 𝑃𝑠𝑢𝑝1 tap. Another pressure tap is put on the right side wall to

measure the pressure𝑃𝑠𝑢𝑝3. Their locations are shown in Figure 6 below.

7

Figure6. The locations of the pressure taps

The removable partition wall is 36 inches long and made of clear acrylic plastic. The

cross section is in a trapezoidal shape. It connects the supply channel and the trailing

edge channel with 11 crossover holes. The first hole locates 8.5 inches from the left hand

side end and other adjacent holes are 2 inches apart from each other. Figure 7 shows the

details of the crossover holes.

17.00” 17.75” 13.25”

48”

8

Figure 7. Details of the cross-over holes (removable partition holes)

The trailing edge channel is the most important part in this experiment. It is 38.5 inches

long and consists five parts: the front wall, the side wall, the removable wall which is

bottom wall, the trailing edge wall and the heater. The front wall of the trailing edge

channel has a rectangular shape while the two side walls are in trapezoidal shape. These

three walls are made of 0.5 inches thick clear acrylic plastic. Two pressure taps are

placed in the middle of the front wall from which the pressure difference of the air before

and after flowing through the turbulator can be solved. Two thermal couples and two

pressure taps are placed on both sides to measure the temperatures 𝑇𝑒𝑛𝑑 1 & 𝑇𝑒𝑛𝑑 2 and

pressures 𝑃𝑒𝑛𝑑 1 & 𝑃𝑒𝑛𝑑 2. The removable wall was introduced before. More details of

trailing edge channel are shown below in figure 8.

Cross section view Upside view

9

Figure 8. Details of the trailing edge channel

The top wall of the trailing edge channel is called trailing edge wall. It is made of the

clear plastic with a trapezoid shape cross section which can be seen from figure 5. This

wall has 12 exit holes where the first hole locates 7.5 inches away from the left hand side

end and other holes are 2 inches apart from each other. Details of the trailing edge exit

holes are shown in figure 9.

Figure 9. Details of the trailing edge holes

10

The back wall part of the trailing edge channel is the heater part which plays a crucial

role in this experiment, because it provides the heat flux to measure the heat transfer

coefficient. The heater part has couples of layers. The first layer is liquid crystal foil upon

which 11 turbulators are pasted. These turbulators are placed at the center line of the

liquid crystal foil right above each crossover holes (see Figure 11). The shape and

dimensions of these turbulators are shown below in Figure 10.

Figure 10. The dimensions of the turbulators used in experiment

Liquid crystal is originally black and will turn to different colors as temperature changes.

At any particular temperature, liquid crystals reflect a single wavelength of light. The

colors can be calibrated to particular temperatures since the transition of color is sharp

and precise. The calibration of this experimental investigation considers an appearance of

specific green shade which corresponds to the temperature of 96.4 ℉. The total thickness

of this liquid crystal foil is 0.001 inch. Under liquid crystal there are three heaters placed

in a row called Heater1, Heater2 and Heater3 from the left to right respectively. Each

11

heater is 11 inches long and 2.5 inches wide. They are connected to a power supply with

8 different channels that controls the voltages across each heater (see Figure 21).

Under three heaters, there is a 3 inches thick polyurethane layer with specific thermal

conductivity which supports the heater and gets rid of the leaking of the air.

A Panasonic Lumix camera was used to take the pictures of the liquid crystal foil in

different temperatures. These photos will be digitalized in 𝑠𝑖𝑔𝑚𝑎 𝑠𝑐𝑎𝑛 𝑝𝑟𝑜5 software.

After digitalizing, the areas of green color in each picture can be quantified, and then the

average Nusselt number is solved.

There are two kinds of holes arrangements in this experiment, that is, inline arrangement

and staggered arrangement. Figure 11 shows inline arrangement while Figure 12 shows

staggered arrangement.

Figure 11. Inline arrangement flow

12

Figure 12. Staggered arrangement flow

As the cross-over holes have two different angles, there are 4 kinds of geometries in this

experiment:

inline arrangement, zero tilt angle

inline arrangement, five tilt angle

staggered arrangement, zero tile angle

staggered arrangement, five tilt angle

And for this test, the camera only focused at the last four turbulators on the right hand

side. This is because the aim of this experiment is to find out the influence of blocked exit

holes on the right side to the heat transfer coefficient.

13

Figure 13. Camera focuses and the four areas for staggered arrangement

Figure 14. Camera focuses and the four areas for inline arrangement

Camera focusing

Area1 Area2 Area3 Area4

Area1 Area2 Area3 Area4

Camera focusing

14

Experimental Procedure

Liquid crystal calibration

In this experiment, the liquid crystal is used to measure the heat transfer coefficient. Thus

the property of the liquid crystal should be known, that is, which color represents what

temperature. Fortunately, only the green color is calibrated in this experiment. This is

because the green color is easy to identify and therefore is chosen to be the reference

color for the liquid crystal. And the temperature it represents is called the reference

temperance. According to the previous researches, the reference temperature of the liquid

crystal is between 90℉ and 100℉. While doing the calibration, one piece of liquid

crystal display sheet was merged in water starting at approximately 100℉. A

thermocouple was used to test the temperature of the surface of the liquid crystal sheet.

Both the temperature displayed on the screen and the color of the liquid crystal sheet

were recorded by a video camera. During the whole process, the water was stirred

carefully to make it cool fast and even. When the temperature dropped to 90℉, the

calibration was done. The reference temperature can be decided from the video taken. For

this experiment, the reference temperature is 94.6℉ which is shown below in Figure 15.

15

Figure 15. Liquid crystal display of the reference color and the reference temperature.

Cold and Heat Transfer Tests

As to get accurate results, the test section must be hermetically sealed. Before running the

test, the silicone was applied to any cracks and seals that were visible. Normally the

silicone needs 24 hours to dry. After that, the compressor was turned on and the air was

allowed to go through the system at a pressure equal or higher than 80 psi. The test was

tested for leaks with a soap-water based method. If any more leaks were found, silicone

was reapplied and let dry for another 24 hours. Once the leakage test had done, the

experiment can be continued.

There are total 16 different geometries in this experiment.

16

Geometry1: 11crossover holes-12 exit holes, inline arrangement, 0 degree tilt angle,

no bleed

Geometry2: 11crossover holes-9 exit holes, inline arrangement, 0 degree tilt angle,

no bleed

Geometry3: 11crossover holes-8exit holes, inline arrangement, 0 degree tilt angle, no

bleed

Geometry4: 11crossover holes-7 exit holes, inline arrangement, 0 degree tilt angle,

no bleed

Geometry5: 11crossover holes-12 exit holes, inline arrangement, 5 degree tilt angle,

no bleed

Geometry6: 11crossover holes-9exit holes, inline arrangement, 5 degree tilt angle, no

bleed

Geometry7: 11crossover holes-8 exit holes, inline arrangement, 5 degree tilt angle,

no bleed

Geometry8: 11crossover holes-7 exit holes, inline arrangement, 5 degree tilt angle,

no bleed

Geometry9: 11crossover holes-12 exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry10: 11crossover holes-10 exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry11: 11crossover holes-9 exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

17

Geometry12: 11crossover holes-8 exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry13: 11crossover holes-12 exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Geometry14: 11crossover holes-10 exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Geometry15: 11crossover holes-9 exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Geometry16: 11crossover holes-8 exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

For each case, two kinds of test are conducted:

Cold Test

Heat Transfer Test

Cold Test:

In the cold test, the experiment set up was running without using the heaters. There are 11

different pressures for cold test: 5, 10, 15, 20, 25, 30, 40, 50, 60, 70, 80 psi. This test was

done at the beginning of each experiment. The original log sheets for the cold tests are

located in Appendix A. The variables taken in both cold and heat transfer tests are

explained below.

Tven: The air temperature at the critical venturi inlet

18

Tin1: The temperature of the air flowing through the bell mouth opening on one

side

Tin2: The temperature of the air flowing through the bell mouth opening on the

opposite side of Tin1

Tjet: The temperature of the air flowing through the channel

Tend1: The temperature of the air at the end of the channel closest to the plenum

Tend2: The temperature of the air at the opposite end of channel

Tamb: Lab temperature

V1 and A1: The voltage and amperage readings from heater 1

V2 and A2: The voltage and amperage readings from heater 2

V3 and A3: The voltage and amperage readings from heater 3

Pplen: The pressure reading from the plenum

Psup1: The pressure reading from the cavity or supply channel closest to the

plenum, also found in Figure 4 above

Psup2: The pressure reading from the cavity or supply channel in the middle of

the section, also found in Figure 4 above

Psup3: The pressure reading from the cavity or supply channel from the opposite

side of Psup1, also found in Figure 4 above

Pend1: The pressure reading from the test section closest to the plenum, also

found in Figure 4 above

Pend2: The pressure reading from the test section opposite to Pend1, also found in

Figure 4 above

DP, orifice: Pressure difference across the orifice plate

19

Pamb: Lab pressure

Cross-Over Hole Angle: Indicates the angle of the cross-over jet toward the target

wall

TE slot arrangement: Indicates whether or not the racetrack exit holes are in line

or staggered with respect to the cross-over holes

Bleed Valve: indicates whether or not the valve is open or closed

Remarks: The comments of that specific experiment

Heat transfer Test:

For this experiment, two heaters were used in the heat transfer test. They are heater 2 and

heater 3. The reason is because that heater 3 is the target zone while heater 2 is used to

get rid of the heat transfer from heater 3 to heater 2 in horizontal direction. Unlike the

cold test, there are 6 different venturi pressures in heat transfer test (13, 26, 40, 54, 69 and

80 psi) corresponding to six jet Reynolds Numbers in each experiment.

When an experiment was chosen to be performed, the compressor was turned on. The

venturi gauge pressure was set to a pre-determined pressure and the system was left on

for approximately 30 minutes for it to reach equilibrium. In the meantime, the heat

exchange system which using cold water was turned on to cool the incoming air. After

the air system got equilibrium, make sure the venturi pressure is correct. Usually the

venturi gauge pressure dropped a little. Then the electrical power panel, volt-meter, amp-

meter, acquisition switch unit and micro-manometer were turned on. The last step before

the data acquisition process was to determine the minimum and maximum voltages for

the heaters. The minimum voltage is the voltage of the heater when the reference green

20

color first shows on the corresponding liquid crystal display sheet. The maximum voltage

is the voltage of the heater when the reference green color is last seen on the liquid

crystal. Then the voltage increment was got by the following formula ∆𝑉 = (𝑉𝑚𝑎𝑥 −

𝑉𝑚𝑖𝑛 )/20 . 20 is the desired number of pictures taken in each experiment. However a

typical experiment would have 18-25 pictures. According to this voltage increment, the

heater progressed from the minimum voltage to the maximum voltage. A Panasonic

Lumix digital camera was placed in front of the testing section focusing on the target

zone which is the last four turbulators. Figure 13 and 14 show the target zone and the

areas.

The temperature was read in degrees Fahrenheit from 6 different channels. See Figure 16.

The relationship between channel number and temperatures are shown below.

Channel 101 reading for Tven

Channel 102 reading for Tjet

Channel 103 reading for Tin1

Channel 104 reading for Tin2

Channel 105 reading for Tend1

Channel 106 reading for Tend2

21

Figure 16. Thermometer used in experiment

Figure 17. True-rms Multimeter used in experiment

22

The lab temperature Tamb was taken by a True-rms Multimeter which is shown in Figure

17.

The pressures were taken by three types of manometers which are listed below.

Micro-manometer Oil’s specific gravity to water is 1.000

Orange-manometer Oil’s specific gravity to water is 0.827

Red-manometer Oil’s specific gravity to water is 2.950

Micro-manometer is for low pressure measure but more accurate. Its accuracy is 0.001

inches of distilled water. Its range is from 0 to 1.000 inches of distilled water. The

reading of Micro-manometer should be multiplied by 2 before used. Orange-manometer

is for medium pressure measure. Its accuracy is 0.1 inches of oil which has a 0.827

specific gravity to distilled water. It’s range is from 0 to 30.00 inches of orange oil. Red-

manometer is for high pressure measure. Its accuracy is 0.1 inches of red oil which has a

2.950 specific gravity to distilled water. It’s range is from 0 to 50.00 inches of red oil.

Figure 18, 19 and 20 show these three types of manometers.

23

Figure 18. Micro-manometer used in experiment

Figure 19. Orange-manometer used in experiment

24

Figure 20. Red-manometer used in experiment

Figure 21. Electrical power panel used in experiment

25

Figure 21 shows the electrical power panel which controls the voltage of the heaters. This

electrical power panel contains eight small rheostats. As two heaters were used in the

experiment, only two small rheostats which are channel 3 and channel 4 were used.

Channel 3 controlled heater 2 while channel 4 controlled heater 3. During the test, the

main knob of the panel was kept at 80 Volt. Channel 3 and 4 were turned to the pre-

solved minimum voltage first, and then for each step, the voltage of heater 3 which is

channel 4 was increased by one voltage increment. Channel 3 which controlled heater 2

was turned to make sure the voltage of heater 2 is equal to that of heater 3. Each picture

of the target zone was taken for each step.

After all pictures were taken, a software 𝑠𝑖𝑔𝑚𝑎 𝑠𝑐𝑎𝑛 𝑝𝑟𝑜5 was used to digitalize them,

the area of the green color for each picture in each area was calculated and put in an excel

log sheet. These area values were used to calculate the average Nusselt Number for each

area.

Below is a summary of what was performed for each experiment.

1. Turn on the compressor to start air flow and keep track of time

2. Turn on the heat exchanger

3. Select the proper pressure from the pressure regulator

4. Wait for approximately 30 minutes for the system to reach operating equilibrium

5. Find the minimum and maximum voltages for the liquid crystal display, and then

determine the voltage increments

6. Start with the minimum voltage, record all of the variables and including the

picture

26

7. Finish with last picture, keep the compressor on to cool the whole system for 30

minutes

8. Start from step 1 again to start the new experiment

9. Using Sigma Scan Pro5 to digitalize the pictures and export the results to an excel

file

27

Data reduction

When all the experiments were completed and all the variables were collected, three

different FORTRAN programs were run. They are check.f, reduce.f and integare.f.

1. Check.f

Check.f program is used to check typographic errors. It read all the data taken in the

experiment and compared them with the reference values. If any data was not in the

specific range of values, it would be considered as a typographic error, and then the

program alerted the user that there was a typing error in the input file. For example, for

pressure 𝑃𝑎𝑚𝑏 , the reference range of value is 28psi to 31psi. So if

𝑃𝑎𝑚𝑏 < 28 𝑜𝑟 𝑃𝑎𝑚𝑏 > 31, it was seen as an error. For voltage and amperage, they were

checked using the equation1 shown below.

𝐸𝑟𝑟𝑜𝑟𝑖 =

𝑉𝑖𝐴𝑖−(

𝑉𝑖𝐴𝐼

)𝑜𝑙𝑑

(𝑉𝑖𝐴𝐼

)𝑜𝑙𝑑 ≤ 0.0125

Where 𝑖 = 1,2,3 for heater 1, 2, 3 respectively. If 𝐸𝑟𝑟𝑜𝑟𝑖 > 0.0125 , the program will

alert the user to check it. The FORTRAN program (check.f) can be found in Appendix B.

2. Reduce.f

After checking for errors, the data was taken to the next step, which is reduce.f program.

The code for reduce.f is shown in Appendix C. This program takes all the values and

calculates the energy balance. The total heat flux corresponding to each heater as well as

(1)

28

the local heat transfer coefficients, the total heat losses to the ambient, radiative fluxes

and the Nusselt number were calculated.

2.1 Geometry calculation

The reduce.f first performed all geometric calculations. Geometries for venturi, heaters,

trailing-edge channel, cross-over slots and exit slots as well as the heat transfer area were

calculated. The hydraulic diameter (𝐷𝑕 ) is determined by 4 times of the cross-section area

divided by the cross-section’s perimeter as shown in equation 2.

𝐷𝑕 =4𝐴𝑐𝑟𝑜𝑠𝑠

𝑃

2.2 Coefficient calcuation

Then the jet Reynolds number is

𝑅𝑒𝑗𝑒𝑡 =𝜌∗𝑣∗𝑆𝑙𝑜𝑡 𝐷𝑕

𝜇 𝑗𝑒𝑡=

4∗𝑚

𝑃𝑒𝑟𝑖𝑚𝑒𝑡𝑒𝑟 ∗𝜇 𝑗𝑒𝑡

Where 𝑚 = 𝜌 ∗ 𝑣 ∗ 𝐴𝑐𝑟𝑜𝑠𝑠 .

The Nusselt number is got by equation 4.

𝑁𝑢𝑗𝑒𝑡 =𝑕𝑡𝑢𝑟𝑏 ∗𝑆𝑙𝑜𝑡 𝐷𝑕

𝐾

Where the 𝑆𝑙𝑜𝑡𝐷𝑕 is the hydraulic diameter of the cross-over slot. 𝐾 is the thermal

conductivity of the air. And 𝑕𝑡𝑢𝑟𝑏 is the heat transfer coefficient which will be solved

later by an energy balance equation.

(2)

(3)

(4)

29

The inlet temperature 𝑇𝑖𝑛 is the average of the 𝑇𝑖𝑛1 and 𝑇𝑖𝑛2. The air flow rate through the

critical venturi is calculated by equation 5 which is the correlation for small critical

venturi.

𝑚 =0.5215∗𝐴𝑣𝑒𝑛 ∗(𝑃𝑣𝑒𝑛 +𝑃𝑎𝑚𝑏 )

𝑇𝑣𝑒𝑛 +460

The total heat added to the air by the heaters from the inlet to the point in question is

solved by equation 6.

𝑄 = 3.412 ∗ ( 𝑉1𝐴1 + 𝑉2𝐴2 + (𝑉3𝐴3))

Where the heat flux 𝑓𝑙𝑢𝑥𝑏 is

𝑄" = 𝐹𝑙𝑢𝑥𝑏 = 3.412 ∗ (𝑉2𝐴2

𝐻𝑒𝑎𝑡𝑒𝑟 𝐴𝑟𝑒𝑎)

This variable will be used in the calculation later.

2.3 Energy balance-Heating resistance calculation

When all the geometries had been calculated, the program came to the energy balance

part. Some variables used in energy balance are listed below.

𝑕0 =0.36∗𝐾𝑎𝑚𝑏

𝐷𝑒

Where 𝐷𝑒 = 7/12,

𝑅𝑐𝑜𝑣 = 1/𝑕0

(5)

(6)

(7)

(8)

(9)

30

Where 𝑅𝑐𝑜𝑣 is the heat resistance of the ambient air,

𝑇𝑚 = 𝑇𝑗𝑒𝑡

Here, 𝑇𝑚 = 𝑇𝑗𝑒𝑡 is used for 𝑕 calculation, not for 𝑇𝑚 calculation which is a few degrees

higher.

In the energy balance, as the horizontal direction heat transfer got eliminated by using the

same voltages for heater2 and heater3, only four directions of heat transfer were

considered: back, front, top and bottom. While calculating the resistances, some

abbreviations were used for convenience. For example, in statement like tadh1/kadh, tadh

means the thickness of adhesive layer while kadh stands for the thermal conductivity of

the adhesive layer. The materials thermal conductivities were got from relative references

and are listed here: 𝑘𝑘𝑎𝑝𝑡𝑜𝑛 = 0.0942𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉, 𝑘𝑝𝑜𝑙𝑦𝑢𝑟𝑒𝑡 𝑕𝑎𝑛𝑒 = 0.033

𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉,

𝑘𝑝𝑙𝑒𝑥𝑖𝑔𝑙𝑎𝑠 = 0.11𝐵𝑇𝑈

𝑕𝑟. 𝑓𝑡.℉, 𝑘𝑚𝑦𝑙𝑎𝑟 = 0.085

𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉, 𝑘𝑎𝑑𝑕𝑒𝑠𝑖𝑣𝑒 = 0.1272

𝐵𝑇𝑈

𝑕𝑟. 𝑓𝑡.℉,

𝑘𝑖𝑛𝑐𝑜𝑛𝑒𝑙 = 9.0152𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉, 𝑘𝑏𝑙𝑎𝑐𝑘𝑔𝑟𝑜𝑢𝑛𝑑 = 0.165

𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉, 𝑘𝑙𝑖𝑞𝑢𝑖𝑑 𝑐𝑟𝑦𝑠𝑡𝑎𝑙 =

0.165𝐵𝑇𝑈

𝑕𝑟.𝑓𝑡.℉.

Back direction-back wall

For the back direction, there was a back wall which is liquid crystal wall. The heating

resistance was calculated from the center of the heating element to the ambient air. There

were couples of layers between the heating element to the ambient air, which are 0.25 mil

inconel heating element, 0.5 mil adhesive, 0.5 mil kapton, 2 mil adhesive, 1.625 inches

polyurethane, 2.0 inches Styrofoam. Their heating resistances are tinc1/kinc, tadh1/kadh,

(10)

31

tkap1/kkap, tadh4/kadh, tpoly/kpoly, tsty/ksty and 1/ho respectively. Thus the total

heating resistance of the back direction was calculated by equation 11 below:

𝑅𝑏𝑎𝑐𝑘 = 0.5 ∗ 𝑅𝑖𝑛𝑐1 + 𝑅𝑎𝑑𝑕1 + 𝑅𝑘𝑎𝑝 1 + 𝑅𝑎𝑑𝑕4 + 𝑅𝑝𝑜𝑙𝑦 + 𝑅𝑐𝑜𝑛𝑣

Where 𝑅𝑖𝑛𝑐1 = 𝑡𝑖𝑛𝑐1/𝑘𝑖𝑛𝑐, 𝑅𝑎𝑑𝑕1 = 𝑡𝑎𝑑𝑕1/𝑘𝑎𝑑𝑕, 𝑅𝑘𝑎𝑝 1 = 𝑡𝑘𝑎𝑝1/𝑘𝑘𝑎𝑝, 𝑅𝑎𝑑𝑕4 =

𝑡𝑎𝑑𝑕4/𝑘𝑎𝑑𝑕, and 𝑅𝑝𝑜𝑙𝑦 = 𝑡𝑝𝑜𝑙𝑦/𝑘𝑝𝑜𝑙𝑦.

Front direction-front direction inside section and front wall

For the front direction, there were two parts of processes. One is from the center of the

heating element to the air inside the test section, and the other is from air inside the test

section to the ambient air. For the first process, the layers are 0.25 mil inconel heating

element, 1.0 mil adhesive, 2.0 mil kapton, 1.0 mil adhesive, 0.5 mil inconel spreader, 1.0

mil adhesive, 2.0 mil kapton, 1.5 mil adhesive, 3.0 mil absorptive black background, 2.0

mil liquid crystal, 5.0 mil mylar and air inside the test section. Their heating resistances

are tinc1/kinc, tadh2/kadh, tkap2/kkap, tadh2/kadh, tinc2/kinc, tadh2/kadh, tkap2/kkap,

tadh3/kadh, tblack/kblack, tliq/kliq, tmyl/kmyl and 1/hi. The second process was air

inside the test section, 0.45 inches Plexiglas and ambient. Where the resistances are 1/hi,

tplex/kplex and 1/ho. Thus the total heating resistance from the heating element center to

the air inside the test section was calculated by equation 12 below:

𝑅𝑓𝑟𝑜𝑛𝑡 = 𝑅𝑖𝑛𝑐1 + 𝑅𝑎𝑑𝑕2 + 𝑅𝑘𝑎𝑝 2 + 𝑅𝑎𝑑𝑕2 + 𝑅𝑖𝑛𝑐2 + 𝑅𝑎𝑑𝑕2 + 𝑅𝑘𝑎𝑝 2 + 𝑅𝑎𝑑𝑕3 + 𝑅𝑏𝑙𝑎𝑐𝑘

+ 𝑅𝑙𝑖𝑞

(11)

(12)

32

Where 𝑅𝑎𝑑𝑕2 = 𝑡𝑎𝑑𝑕2/𝑘𝑎𝑑𝑕, 𝑅𝑘𝑎𝑝 2 = 𝑡𝑘𝑎𝑝2/𝑘𝑘𝑎𝑝, 𝑅𝑖𝑛𝑐2 = 𝑡𝑖𝑛𝑐2/𝑘𝑖𝑛𝑐, 𝑅𝑎𝑑𝑕2 =

𝑡𝑎𝑑𝑕3/𝑘𝑎𝑑𝑕, 𝑅𝑏𝑙𝑎𝑐𝑘 = 𝑡𝑏𝑙𝑎𝑐𝑘/𝑘𝑏𝑙𝑎𝑐𝑘 and 𝑅𝑙𝑖𝑞 = 𝑡𝑙𝑖𝑞/𝑘𝑙𝑖𝑞.

And the heating resistance for the front wall which is from the air inside the test section

to the ambient air was calculated by:

𝑅1 = 𝑅𝑝𝑙𝑒𝑥 + 𝑅𝑐𝑜𝑣

Where 𝑅𝑝𝑙𝑒𝑥 = 𝑡𝑝𝑙𝑒𝑥/𝑘𝑝𝑙𝑒𝑥.

Top direction-top wall

For the top wall,

𝑅𝑡𝑜𝑝 = 𝑅𝑝𝑙𝑒𝑥 + 𝑅𝑐𝑜𝑛𝑣

Bottom direction-bottom wall

For the bottom wall,

𝑅𝑏𝑜𝑡 = 𝑅𝑝𝑙𝑒𝑥 + 𝑅𝑠𝑡𝑦 + 𝑅𝑐𝑜𝑣

2.4 energy balance-heat flux calculation

The heat flux for all four directions is shown below:

𝐹𝑙𝑢𝑥𝑡𝑜𝑝 = 0

𝐹𝑙𝑢𝑥𝑓 = 0

𝐹𝑙𝑢𝑥𝑏𝑜𝑡 = 0

(13)

(16)

(17)

(18)

(14)

(15)

33

And

𝐹𝑙𝑢𝑥𝑏 = 3.412 ∗ (𝑉2𝐴2

𝐻𝑒𝑎𝑡𝑒𝑟 𝐴𝑟𝑒𝑎)

see equation 7.

Then the temperature at the center of the heating element was found by equation 17:

𝑇𝑕𝑒𝑎𝑡𝑒𝑟 =𝐹𝑙𝑢𝑥𝑏 +

𝑇𝑙𝑖𝑞𝑢𝑖𝑑

𝑅𝑓𝑟𝑜𝑛𝑡+

𝑇𝑎𝑚𝑏𝑅𝑏𝑎𝑐𝑘

1

𝑅𝑏𝑎𝑐𝑘+

1

𝑅𝑓𝑟𝑜𝑛𝑡

Where 𝑇𝑙𝑖𝑞𝑢𝑖𝑑 is the reference temperature of the liquid crystal.

2.5 energy balance-heat losses calculation

When the heat resistances and heat flux for all four directions were solved, the losses

were considered.

Back direction-back wall

The loss from back wall 𝐹𝑙𝑏𝑎𝑐𝑘 was

𝐹𝑙𝑏𝑎𝑐𝑘 = (𝑇𝑕𝑒𝑎𝑡𝑒𝑟 − 𝑇𝑎𝑚𝑏𝑖𝑒𝑛𝑡 )/𝑅𝑏𝑎𝑐𝑘

Front direction-front direction inside the test section

While the loss for front side inside the section 𝐹𝑓𝑟𝑜𝑛𝑡 was

𝐹𝑓𝑟𝑜𝑛𝑡 = (𝑇𝑕𝑒𝑎𝑡𝑒𝑟 − 𝑇𝑙𝑖𝑞𝑢𝑖𝑑 )/𝑅𝑓𝑟𝑜𝑛𝑡

(19)

(20)

(21)

34

Then the back wall temperature 𝑇𝑏𝑎𝑐𝑘 , the film temperature 𝑇𝑓 and the percentage of heat

loss 𝐻𝑒𝑎𝑡𝑝𝑒𝑟𝑙𝑜𝑠𝑠 can be solved by equations below

𝑇𝑏𝑎𝑐𝑘 = 𝑇𝑙𝑖𝑞𝑢𝑖𝑑 − 𝐹𝑓𝑟𝑜𝑛𝑡 ∗ 𝑅𝑚𝑦1

𝑇𝑓 = 0.5 ∗ (𝑇𝑚 + 𝑇𝑏𝑎𝑐𝑘 )

𝐻𝑒𝑎𝑡𝑝𝑒𝑟𝑙𝑜𝑠𝑠 = 100 ∗ (𝐹𝑙𝑏𝑎𝑐𝑘 /𝑄") = 100 ∗ (𝐹𝑙𝑏𝑎𝑐𝑘 /𝐹𝑙𝑢𝑥𝑏)

Top direction-top wall

For the top wall, set 𝑇𝑡𝑜𝑝 = 𝑇𝑚 , and the loss of energy was found by

𝐹𝑙𝑡𝑜𝑝 = (𝑇𝑡𝑜𝑝 − 𝑇𝑎𝑚𝑏 )/𝑅𝑡𝑜𝑝

Bottom direction-bottom wall

For the bottom, set 𝑇𝑏𝑜𝑡 = 𝑇𝑖𝑛 , then the loss from bottom was solved

𝐹𝑙𝑏𝑜𝑡 = (𝑇𝑏𝑜𝑡 − 𝑇𝑎𝑚𝑏 )/𝑅𝑏𝑜𝑡

Front direction-front wall

For the front wall, the temperature 𝑇𝑓𝑟𝑜𝑛𝑡 and the loss 𝐹𝑙𝑓𝑟𝑜𝑛𝑡 were both unknown.

However, both of them are important for solving the heat transfer coefficient 𝑕𝑡𝑢𝑟𝑏 . To

solve this problem, Newton’s method was used.

(23)

(24)

(22)

(25)

(26)

35

2.6 Newton’s method

The program first gave an initial guess for 𝑕𝑡𝑢𝑟𝑏 and 𝑇𝑓𝑟𝑜𝑛𝑡 , then using the relation of

radiation heat loss to solve for new value of 𝑇𝑓𝑟𝑜𝑛𝑡 that is 𝑇𝑓𝑟𝑜𝑛𝑡𝑁 . And if 𝑇𝑓𝑟𝑜𝑛𝑡𝑁

satisfied the convergence condition, then set 𝑇𝑓𝑟𝑜𝑛𝑡 = 𝑇𝑓𝑟𝑜𝑛𝑡𝑁 . After this, the heat

transfer coefficient 𝑕𝑡𝑢𝑟𝑏 can be solved.

Initial guesses

𝑕𝑏𝑎𝑐𝑘 = (𝐹𝑙𝑢𝑥𝑏 − 𝐹𝑙𝑏𝑎𝑐𝑘 )/(𝑇𝑏𝑎𝑐𝑘 − 𝑇𝑚)

𝑕𝑓𝑟𝑜𝑛𝑡 = 𝑕𝑏𝑎𝑐𝑘

𝑇𝑓𝑟𝑜𝑛𝑡 = 𝑇𝑚

Here 𝑕𝑡𝑢𝑟𝑏 = 𝑕𝑏𝑎𝑐𝑘 which was not a guess.

And the convective resistance 𝑅3 is equal to 1/𝑕𝑓𝑟𝑜𝑛𝑡 which was also a truth.

Solve for new value of 𝑻𝒇𝒓𝒐𝒏𝒕

From the radiation loss equation,

𝑇𝑓𝑟𝑜𝑛𝑡𝑁 =(

1

𝑅3 ∗𝑇𝑚 +

1

𝑅1 ∗𝑇𝑎𝑚𝑏 −𝐹𝑟𝑓𝑟𝑜𝑛𝑡 )

(1

𝑅1+

1

𝑅3)

Convergence condition

If 𝑇𝑓𝑟𝑜𝑛𝑡 − 𝑇𝑓𝑟𝑜𝑛𝑡𝑁 ≤ 0.001, then 𝑇𝑓𝑟𝑜𝑛𝑡 = 𝑇𝑓𝑟𝑜𝑛𝑡𝑁 .

(29)

(28)

(27)

(30)

36

2.7 solve for heat transfer coefficient

For the front wall,

𝐹𝑙𝑓𝑟𝑜𝑛𝑡 = (𝑇𝑓𝑟𝑜𝑛𝑡 − 𝑇𝑎𝑚𝑏 )/𝑅1

Then the total heat loss to the ambient air via radiation and conduction can be quantified,

𝑄𝑤𝑎𝑠𝑡𝑒𝑑 = 𝐹𝑙𝑡𝑜𝑝 ∗ 𝐴𝑡𝑜𝑝 + 𝐹𝑙𝑏𝑜𝑡 ∗ 𝐴𝑏𝑜𝑡 + 𝐹𝑙𝑓𝑟𝑜𝑛𝑡 ∗ 𝐴𝑓𝑟𝑜𝑛𝑡 + 𝐹𝑙𝑏𝑎𝑐𝑘 ∗ 𝐴𝑏𝑎𝑐𝑘

Then, the net heat added to the from the inlet to the point in question is solved by,

𝑄𝑎𝑑𝑑 = 𝑄 − 𝑄𝑤𝑎𝑠𝑡𝑒

From the Newton law of cooling, the heat transfer coefficient can be found

𝑕𝑏𝑎𝑐𝑘 =𝐹𝑙𝑢𝑥𝑏 −𝐹𝑙𝑏𝑎𝑐𝑘 −𝐹𝑟𝑏𝑎𝑐𝑘

𝑇𝑏𝑎𝑐𝑘 −𝑇𝑚

Then 𝑕𝑡𝑢𝑟𝑏 = 𝑕𝑏𝑎𝑐𝑘 , using equation 4, the Nusselt number for the all target wall can be

quantified.

2.8 uncertainty calculation

The uncertainty for the entire experiment was found by using Kline and McClintock’s

method, and with help from further reading from Robert J Moffat [4].

(30)

(31)

(32)

(33)

37

3. Integarea.f

To find the area weighted average of the Nusselt number, integarea.f program was used.

The average Nusselt number was calculated with equation 34, where A is the pixel area

of the reference color from Sigma Scan Pro for each picture and n is the number of

pictures per experiment.

𝑁𝑢 = 𝑁𝑢𝑖 ∗ 𝐴𝑖

𝑖=𝑛𝑖=1

𝐴𝑖𝑖=𝑛𝑖=1

The source code for integare.f can be found in Appendix D.

After these three programs, graphs were made and analyzed.

(34)

38

Results and Discussion

In this experiment, the purpose is to find the influence of blocked exit holes to the

average heat transfer coefficient. For each crossover holes tilt angle and exit holes

arrangement, there are four different cases. These 16 different cases were conducted and

compared.

All these arrangements were for closed bleed valve.

These cases are shown below:

Geometry1: 11crossover holes-12exit holes, inline arrangement, 0 degree tilt angle,

no bleed

Geometry2: 11crossover holes-9exit holes, inline arrangement, 0 degree tilt angle, no

bleed

Geometry3: 11crossover holes-8exit holes, inline arrangement, 0 degree tilt angle, no

bleed

Geometry4: 11crossover holes-7exit holes, inline arrangement, 0 degree tilt angle, no

bleed

Geometry5: 11crossover holes-12exit holes, inline arrangement, 5 degree tilt angle,

no bleed

Geometry6: 11crossover holes-9exit holes, inline arrangement, 5 degree tilt angle, no

bleed

Geometry7: 11crossover holes-8exit holes, inline arrangement, 5 degree tilt angle, no

bleed

Geometry8: 11crossover holes-7exit holes, inline arrangement, 5 degree tilt angle, no

bleed

Geometry9: 11crossover holes-12exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry10: 11crossover holes-10exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry11: 11crossover holes-9exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry12: 11crossover holes-8exit holes, staggered arrangement, 0 degree tilt

angle, no bleed

Geometry13: 11crossover holes-12exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Geometry14: 11crossover holes-10exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

39

Geometry15: 11crossover holes-9exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Geometry16: 11crossover holes-8exit holes, staggered arrangement, 5 degree tilt

angle, no bleed

Table 1 below gives the details of these sixteen geometries.

Geometry Arrangement Tilt

angle

(degree)

Number

of

Cross-

over

holes

Number

of exit

holes

Remarks

1 Inline 0 11 12 Reference

2 Inline 0 11 9 Truly inline 2 blocked

3 Inline 0 11 8 Truly inline 3 blocked

4 Inline 0 11 7 Truly inline 4 blocked

5 Inline 5 11 12 Reference

6 Inline 5 11 9 Truly inline 2 blocked

7 Inline 5 11 8 Truly inline 3 blocked

8 Inline 5 11 7 Truly inline 4 blocked

9 Staggered 0 11 12 Reference

10 Staggered 0 11 10 Truly staggered 2 blocked

11 Staggered 0 11 9 Truly staggered 3 blocked

12 Staggered 0 11 8 Truly staggered 4 blocked

13 Staggered 5 11 12 Reference

14 Staggered 5 11 10 Truly staggered 2 blocked

15 Staggered 5 11 9 Truly staggered 3 blocked

16 Staggered 5 11 8 Truly staggered 4 blocked

Table 1. Sixteen different geometries in this experiment

As listed in Table 1, for the same arrangement and tilt angle, the 11cross-over holes 12

exit holes cases served as references. Other cases were compared with these references to

find out the influence of blocked exit holes to the average Nusselt number on the target

zone.

During the test, the camera was only focusing on the last four exit holes, that is, the last

four turbulators on the right hand side of the test section. Four areas were classified on

40

the liquid crystal surface according to these turbulators, namely, area1, area2, area3, and

area4 from left to right. After data reduction, the average heat transfer coefficient and

Reynolds numbers for each area were found and compared. Detail sketches are shown in

Figure 13 and 14.

The graphs below are showing the results

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-12, all open

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 22. Nusselt Number versus Reynolds Number for geometry 1 (11crossover holes-

12 exit holes, inline arrangement, 0 degree tilt angle case) at different pressure

increments.

41

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 23. Nusselt Number versus Reynolds Number for geometry 2 (11crossover holes-

9 exit holes, inline arrangement, 0 degree tilt angle case) at different pressure increments.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 24. Nusselt Number versus Reynolds Number for geometry 3 (11crossover holes-

8 exit holes, inline arrangement, 0 degree tilt angle case) at different pressure increments.

42

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-7, 5 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 25. Nusselt Number versus Reynolds Number for geometry 4 (11crossover holes-

7 exit holes, inline arrangement, 0 degree tilt angle case) at different pressure increments.

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-12, all open

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 26. Nusselt Number versus Reynolds Number for geometry 5 (11crossover holes-

12 exit holes, inline arrangement, 5 degree tilt angle case) at different pressure

increments.

43

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

185

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 27. Nusselt Number versus Reynolds Number for geometry 6 (11crossover holes-

9 exit holes, inline arrangement, 5 degree tilt angle case) at different pressure increments.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 28. Nusselt Number versus Reynolds Number for geometry 7 (11crossover holes-

8 exit holes, inline arrangement, 5 degree tilt angle case) at different pressure increments.

44

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

185

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-7, 5 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 29. Nusselt Number versus Reynolds Number for geometry 8 (11crossover holes-

7 exit holes, inline arrangement, 5 degree tilt angle case) at different pressure increments.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-12, all open

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 30. Nusselt Number versus Reynolds Number for geometry 9 (11crossover holes-

12 exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments.

45

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-10, 2 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 31. Nusselt Number versus Reynolds Number for geometry 10 (11crossover

holes-10 exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-9, 3 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 32. Nusselt Number versus Reynolds Number for geometry 11(11crossover holes-

9 exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments.

46

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 0 degree, 11-8, 4 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 33. Nusselt Number versus Reynolds Number for geometry 12(11crossover holes-

8 exit holes, staggered arrangement, 0 degree tilt angle case) at different pressure

increments.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-12, all open

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 34. Nusselt Number versus Reynolds Number for geometry 13 (11crossover

holes-12 exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments.

47

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

190

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-10, 2 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 35. Nusselt Number versus Reynolds Number for geometry 14 (11crossover

holes-10 exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 36. Nusselt Number versus Reynolds Number for geometry 15 (11crossover

holes-9 exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments.

48

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 5 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 37. Nusselt Number versus Reynolds Number for geometry 16(11crossover holes-

8 exit holes, staggered arrangement, 5 degree tilt angle case) at different pressure

increments.

25

35

45

55

65

75

85

95

105

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-12, all open

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 38. Nusselt Number versus Reynolds Number of four areas for geometry 1

(11crossover holes-12 exit holes, inline arrangement, 0 degree tilt angle) case.

49

10

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-9, 3 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 39. Nusselt Number versus Reynolds Number of four areas for geometry 2

(11crossover holes-9 exit holes, inline arrangement, 0 degree tilt angle) case.

15

25

35

45

55

65

75

85

95

105

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-8, 4 holes blocked

Nu Vs Re Area1

Nu Vs Re Area2

Nu Vs Re Area3

Nu Vs Re Area4

Figure 40. Nusselt Number versus Reynolds Number of four areas for geometry 3

(11crossover holes-8 exit holes, inline arrangement, 0 degree tilt angle) case.

50

10

20

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-7, 5 holes blocked

Nu Vs Re Area1

Nu Vs Re Area2

Nu Vs Re Area3

Nu Vs Re Area4

Figure 41. Nusselt Number versus Reynolds Number of four areas for geometry 4

(11crossover holes-7 exit holes, inine arrangement, 0 degree tilt angle) case.

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-12, all open

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 42. Nusselt Number versus Reynolds Number of four areas for geometry 5

(11crossover holes-12 exit holes, inline arrangement, 5 degree tilt angle) case.

51

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-9, 3 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 43. Nusselt Number versus Reynolds Number of four areas for geometry 6

(11crossover holes-9 exit holes, inline arrangement, 5 degree tilt angle) case.

15

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-8, 4 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 44. Nusselt Number versus Reynolds Number of four areas for geometry 7

(11crossover holes-8 exit holes, inline arrangement, 5 degree tilt angle) case.

52

10

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-7, 5 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 45. Nusselt Number versus Reynolds Number of four areas for geometry 8

(11crossover holes-7 exit holes, inline arrangement, 5 degree tilt angle) case.

25

35

45

55

65

75

85

95

105

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-12, all open

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 46. Nusselt Number versus Reynolds Number of four areas for geometry 9

(11crossover holes-12 exit holes, staggered arrangement, 0 degree tilt angle) case.

53

15

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-10, 2 blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 47. Nusselt Number versus Reynolds Number of four areas for geometry 10

(11crossover holes-10 exit holes, staggered arrangement, 0 degree tilt angle) case.

15

25

35

45

55

65

75

85

95

105

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-9, 3 blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 48. Nusselt Number versus Reynolds Number of four areas for geometry 11

(11crossover holes-9 exit holes, staggered arrangement, 0 degree tilt angle) case.

54

10

20

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 0 degree, 11-8, 4 blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 49. Nusselt Number versus Reynolds Number of four areas for geometry 12

(11crossover holes-8 exit holes, staggered arrangement, 0 degree tilt angle) case.

30

40

50

60

70

80

90

100

110

120

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-12, all open

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 50. Nusselt Number versus Reynolds Number of four areas for geometry 13

(11crossover holes-12 exit holes, staggered arrangement, 5 degree tilt angle) case.

55

35

45

55

65

75

85

95

105

115

125

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-10, 2 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 51. Nusselt Number versus Reynolds Number of four areas for geometry 14

(11crossover holes-10 exit holes, staggered arrangement, 5 degree tilt angle) case.

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-9, 3 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 52. Nusselt Number versus Reynolds Number of four areas for geometry 15

(11crossover holes-9 exit holes, staggered arrangement, 5 degree tilt angle) case.

56

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 5 degree, 11-8, 4 holes blocked

Nu Vs Re Area 1

Nu Vs Re Area 2

Nu Vs Re Area 3

Nu Vs Re Area 4

Figure 53. Nusselt Number versus Reynolds Number of four areas for geometry 16

(11crossover holes-8 exit holes, staggered arrangement, 5 degree tilt angle) case.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-12, all open

Area 1

Area 2

Area 3

Area 4

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 54. Nusselt Number versus Reynolds Number for geometry 1 (11crossover holes-

12 exit holes, inline arrangement, 0 degree tilt angle) case.

57

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 55. Nusselt Number versus Reynolds Number for geometry 2 (11crossover holes-

9 exit holes, inline arrangement, 0 degree tilt angle) case.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 56. Nusselt Number versus Reynolds Number for geometry 3 (11crossover holes-

8 exit holes, inline arrangement, 0 degree tilt angle) case.

58

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 0 degree, 11-7, 5 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 57. Nusselt Number versus Reynolds Number for geometry 4 (11crossover holes-

7 exit holes, inline arrangement, 0 degree tilt angle) case.

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-12, all open

Area 1

Area 2

Area 3

Area 4

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 58. Nusselt Number versus Reynolds Number for geometry 5 (11crossover holes-

12 exit holes, inline arrangement, 5 degree tilt angle) case.

59

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

185

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 59. Nusselt Number versus Reynolds Number for geometry 6 (11crossover holes-

9 exit holes, inline arrangement, 5 degree tilt angle) case.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 60. Nusselt Number versus Reynolds Number for geometry 7 (11crossover holes-

8 exit holes, inline arrangement, 5 degree tilt angle) case.

60

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

185

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Inline arrangement, 5 degree, 11-7, 5 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 61. Nusselt Number versus Reynolds Number for geometry 8 (11crossover holes-

7 exit holes, inline arrangement, 5 degree tilt angle) case.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

175

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-12, all open

Area 1

Area 2

Area 3

Area 4

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 62. Nusselt Number versus Reynolds Number for geometry 9 (11crossover holes-

12 exit holes, staggered arrangement, 0 degree tilt angle) case.

61

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-10, 2 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 63. Nusselt Number versus Reynolds Number for geometry 10 (11crossover

holes-10 exit holes, staggered arrangement, 0 degree tilt angle) case.

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

165

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 0 degree, 11-9, 3 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 64. Nusselt Number versus Reynolds Number for geometry 11 (11crossover

holes-9 exit holes, staggered arrangement, 0 degree tilt angle) case.

62

5

15

25

35

45

55

65

75

85

95

105

115

125

135

145

155

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 0 degree, 11-8, 4 blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 65. Nusselt Number versus Reynolds Number for geometry 12 (11crossover

holes-8 exit holes, staggered arrangement, 0 degree tilt angle) case.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-12, all open

Area 1

Area 2

Area 3

Area 4

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Figure 66. Nusselt Number versus Reynolds Number for geometry 13 (11crossover

holes-12 exit holes, staggered arrangement, 5 degree tilt angle) case.

63

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

190

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-10, 2 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 67. Nusselt Number versus Reynolds Number for geometry 14 (11crossover

holes-10 exit holes, staggered arrangement, 5 degree tilt angle) case.

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Staggered arrangement, 5 degree, 11-9, 3 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 68. Nusselt Number versus Reynolds Number for geometry 15 (11crossover

holes-9 exit holes, staggered arrangement, 5 degree tilt angle) case.

64

10

20

30

40

50

60

70

80

90

100

110

120

130

140

150

160

170

180

5000 10000 15000 20000 25000 30000 35000 40000

Staggered arrangement, 5 degree, 11-8, 4 holes blocked

13 psi

26 psi

40 psi

54 psi

69 psi

80 psi

Area 1

Area 2

Area 3

Area 4

Figure 69. Nusselt Number versus Reynolds Number for geometry 16 (11crossover

holes-8 exit holes, staggered arrangement, 5 degree tilt angle) case.

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 1 for inline 0 with different number of exit holes

Area 1 for Inline 0, 11-12 all open

Area 1 for Inline 0, 11-9 3blocked

Area 1 for Inline 0, 11-8 4 blocked

Area 1 for Inline 0, 11-7 5 blocked

Figure 70. Nusselt Number versus Reynolds Number for Area 1 at different number of

exit holes cases (inline arrangement, zero degree tilt angle)

65

25

35

45

55

65

75

85

95

105

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 2 for inline 0 with different number of exit holes

Area 2 for Inline 0, 11-12 all open

Area 2 for Inline 0, 11-9 3 blocked

Area 2 for Inline 0, 11-8 4 blocked

Area 2 for Inline 0, 11-7 5 blocked

Figure 71. Nusselt Number versus Reynolds Number for Area 2 at different number of

exit holes cases (inline arrangement, zero degree tilt angle)

15

25

35

45

55

65

75

85

95

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 3 for inline 0 with different number of exit holes

Area3 for Inline 0, 11-12 all open

Area3 for Inline 0, 11-9 3 blocked

Area3 for Inline 0, 11-8 4 blocked

Area3 for Inline 0, 11-7 5 blocked

Figure 72. Nusselt Number versus Reynolds Number for Area 3 at different number of

exit holes cases (inline arrangement, zero degree tilt angle)

66

15

25

35

45

55

65

75

85

95

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 4 for inline 0 with different number of exit holes

Area4 for Inline 0, 11-12 all open

Area4 for Inline 0, 11-9 3 blocked

Area4 for Inline 0, 11-8 4 blocked

Area4 for Inline 0, 11-7 5 blocked

Figure 73. Nusselt Number versus Reynolds Number for Area 3 at different number of

exit holes cases (inline arrangement, zero degree tilt angle)

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 1 for inline 5 with different number of exit holes

Area 1 for inline 5, 11-12 all open

Area 1 for inline 5, 11-9 3 blocked

Area 1 for inline 5, 11-8 4 blocked

Area 1 for inline 5, 11-7 5 blocked

Figure 74. Nusselt Number versus Reynolds Number for Area 1 at different number of

exit holes cases (inline arrangement, five degree tilt angle)

67

20

30

40

50

60

70

80

90

100

110

120

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 2 for inline 5 with different number of exit holes

Area 2 for inline 5, 11-12 all open

Area 2 for inline 5, 11-9 3 blocked

Area 2 for inline 5, 11-8 4 blocked

Area 2 for inline 5, 11-7 5 blocked

Figure 75. Nusselt Number versus Reynolds Number for Area 2 at different number of

exit holes cases (inline arrangement, five degree tilt angle)

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 3 for inline 5 with different number of exit holes

Area 3 for inline 5, 11-12 all open

Area 3 for inline 5, 11-9 3 blocked

Area 3 for inline 5, 11-8 4 blocked

Area 3 for inline 5, 11-7 5 blocked

Figure 76. Nusselt Number versus Reynolds Number for Area 3 at different number of

exit holes cases (inline arrangement, five degree tilt angle)

68

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 4 for inline 5 with different number of exit holes

Area 4 for inline 5, 11-12 all open

Area 4 for inline 5, 11-9 3 blocked

Area 4 for inline 5, 11-8 4 blocked

Area 4 for inline 5, 11-7 5 blocked

Figure 77. Nusselt Number versus Reynolds Number for Area 4 at different number of

exit holes cases (inline arrangement, five degree tilt angle)

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 1 for staggered 0 with different number of exit holes

Area1 for staggered 0. 11-12 all open

Area1 for staggered 0, 11-10 2 blocked

Area1 for staggered 0, 11-9 3 blocked

Area1 for staggered 0, 11-8 4 blocked

Figure 78. Nusselt Number versus Reynolds Number for Area 1 at different number of

exit holes cases (staggered arrangement, zero degree tilt angle)

69

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 2 for staggered 0 with different number of exit holes

Area2 for staggered 0. 11-12 all open

Area2 for staggered 0, 11-10 2 blocked

Area2 for staggered 0, 11-9 3 blocked

Area2 for staggered 0, 11-8 4 blocked

Figure 79. Nusselt Number versus Reynolds Number for Area 2 at different number of

exit holes cases (staggered arrangement, zero degree tilt angle)

15

25

35

45

55

65

75

85

95

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 3 for staggered 0 with different number of exit holes

Area3 for staggered 0. 11-12 all open

Area3 for staggered 0, 11-10 2 blocked

Area3 for staggered 0, 11-9 3 blocked

Area3 for staggered 0, 11-8 4 blocked

Figure 80. Nusselt Number versus Reynolds Number for Area 3 at different number of

exit holes cases (staggered arrangement, zero degree tilt angle)

70

15

25

35

45

55

65

75

85

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 4 for staggered 0 with different number of exit holes

Area4 for staggered 0. 11-12 all open

Area4 for staggered 0, 11-10 2 blocked

Area4 for staggered 0, 11-9 3 blocked

Area4 for staggered 0, 11-8 4 blocked

Figure 81. Nusselt Number versus Reynolds Number for Area 4 at different number of

exit holes cases (staggered arrangement, zero degree tilt angle)

30

40

50

60

70

80

90

100

110

120

130

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 1 for staggered 5 with different number of exit holes

Area 1 for staggered 5, 11-12 all open

Area 1 for staggered 5, 11-10 2 blocked

Area 1 for staggered 5, 11-9 3 blocked

Area 1 for staggered 5, 11-8 4 blocked

Figure 82. Nusselt Number versus Reynolds Number for Area 1 at different number of

exit holes cases (staggered arrangement, five degree tilt angle)

71

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 2 for staggered 5 with different number of exit holes

Area 2 for staggered 5, 11-12 all open

Area 2 for staggered 5, 11-10 2 blocked

Area 2 for staggered 5, 11-9 3 blocked

Area 2 for staggered 5, 11-8 4 blocked

Figure 83. Nusselt Number versus Reynolds Number for Area 2 at different number of

exit holes cases (staggered arrangement, five degree tilt angle)

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 3 for staggered 5 with different number of exit holes

Area 3 for staggered 5, 11-12 all open

Area 3 for staggered 5, 11-10 2 blocked

Area 3 for staggered 5, 11-9 3 blocked

Area 3 for staggered 5, 11-8 4 blocked

Figure 84. Nusselt Number versus Reynolds Number for Area 3 at different number of

exit holes cases (staggered arrangement, five degree tilt angle)

72

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 4 for staggered 5 with different number of exit holes

Area 4 for staggered 5, 11-12 all open

Area 4 for staggered 5, 11-10 2 blocked

Area 4 for staggered 5, 11-9 3 blocked

Area 4 for staggered 5, 11-8 4 blocked

Figure 85. Nusselt Number versus Reynolds Number for Area 4 at different number of

exit holes cases (staggered arrangement, five degree tilt angle)

25

35

45

55

65

75

85

95

105

115

125

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 1 for different arrangement of 11cross-12exit

Area1 for inline 0, all open

Area1 for inline 5, all open

Area1 for staggered 0, all open

Area 1 for staggered 5, all open

Figure 86. Nu Vs Re (Area 1 for different arrangement of 11crossover holes-12exit holes)

73

25

35

45

55

65

75

85

95

105

115

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 2 for different arrangement of 11cross-12exit

Area2 for inline 0, all open

Area2 for inline 5, all open

Area2 for staggered 0, all open

Area 2 for staggered 5, all open

Figure 87. Nu Vs Re (Area 2 for different arrangement of 11crossover holes-12exit holes)

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 3 for different arrangement of 11cross-12exit

Area3 for inline 0, all open

Area3 for inline 5, all open

Area3 for staggered 0, all open

Area 3 for staggered 5, all open

Figure 88. Nu Vs Re (Area 3 for different arrangement of 11crossover holes-12exit holes)

74

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area 4 for different arrangement of 11cross-12exit

Area4 for inline 0, all open

Area4 for inline 5, all open

Area4 for staggered 0, all open

Area 4 for staggered 5, all open

Figure 89. Nu Vs Re (Area 4 for different arrangement of 11crossover holes-12exit holes)

30

40

50

60

70

80

90

100

110

120

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for staggered arrangement 11-10

Area1 for staggered 0, 11cross-10exit

Area 1 for staggered 5, 11cross-10exit

Figure 90. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-10exit holes)

75

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for staggered arrangement 11-10

Area2 for staggered 0, 11cross-10exit

Area 2 for staggered 5, 11cross-10exit

Figure 91. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-10exit holes)

20

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for staggered arrangement 11-10

Area3 for staggered 0, 11cross-10exit

Area3 for staggered 5, 11cross-10exit

Figure 92. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-10exit holes)

76

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for staggered arrangement 11-10

Area4 for staggered 0, 11cross-10exit

Area4 for staggered 5, 11cross-10exit

Figure 93. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-10exit holes)

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for inline arrangement of 11cross 9exit

Area1 for inline 0, 11cross-9exit

Area 1 for inline 5, 11cross-9exit

Figure 94. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-9exit holes)

77

20

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for inline arrangement of 11cross 9exit

Area2 for inline 0, 11cross-9exit

Area 2 for inline 5, 11cross-9exit

Figure 95. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-9exit holes)

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for inline arrangement of 11cross 9exit

Area3 for inline 0, 11cross-9exit

Area3 for inline 5, 11cross-9exit

Figure 96. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-9exit holes)

78

20

30

40

50

60

70

80

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for inline arrangement of 11cross 9exit

Area4 for inline 0, 11cross-9exit

Area4 for inline 5, 11cross-9exit

Figure 97. Nu Vs Re (Area 4 for inline arrangement 11crossover holes-9exit holes)

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for staggered arrangement 11-9

Area1 for staggered 0, 11cross-9exit

Area 1 for staggered 5, 11cross-9exit

Figure 98. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-9exit holes)

79

20

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for staggered arrangement 11-9

Area2 for staggered 0, 11cross-9exit

Area2 for staggered 5, 11cross-9exit

Figure 99. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-9exit holes)

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for staggered arrangement 11-9

Area3 for staggered 0, 11cross-9exit

Area3 for staggered 5, 11cross-9exit

Figure 100. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-9exit holes)

80

15

25

35

45

55

65

75

85

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for staggered arrangement 11-9

Area4 for staggered 0, 11cross-9exit

Area4 for staggered 5, 11cross-9exit

Figure 101. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-9exit holes)

30

40

50

60

70

80

90

100

110

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for inline arrangement of 11cross 8exit

Area1 for inline 0, 11cross-8exit

Area 1 for inline 5, 11cross-8exit

Figure 102. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-8exit holes)

81

20

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for inline arrangement of 11cross 8exit

Area2 for inline 0, 11cross-8exit

Area2 for inline 5, 11cross-8exit

Figure 103. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-8exit holes)

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for inline arrangement of 11cross 8exit

Area3 for inline 0, 11cross-8exit

Area3 for inline 5, 11cross-8exit

Figure 104. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-8exit holes)

82

15

25

35

45

55

65

75

85

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for inline arrangement of 11cross 8exit

Area4 for inline 0, 11cross-8exit

Area4 for inline 5, 11cross-8exit

Figure 105. Nu Vs Re (Area 4 for inline arrangement 11crossover-8exit holes)

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for staggered arrangement 11-8

Area 1 for staggered 0, 11cross-8exit

Area1 for staggered 5, 11cross-8exit

Figure 106. Nu Vs Re (Area 1 for staggered arrangement 11crossover holes-8exit holes)

83

20

30

40

50

60

70

80

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for staggered arrangement 11-8

Area 2 for staggered 0, 11cross-8exit

Area2 for staggered 5, 11cross-8exit

Figure 107. Nu Vs Re (Area 2 for staggered arrangement 11crossover holes-8exit holes)

20

30

40

50

60

70

80

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for staggered arrangement 11-8

Area3 for staggered 0, 11cross-8exit

Area 3 for staggered 5, 11cross-8exit

Figure 108. Nu Vs Re (Area 3 for staggered arrangement 11crossover holes-8exit holes)

84

15

25

35

45

55

65

75

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for staggered arrangement 11-8

Area4 for staggered 0, 11cross-8exit

Area 4 for staggered 5, 11cross-8exit

Figure 109. Nu Vs Re (Area 4 for staggered arrangement 11crossover holes-8exit holes)

30

40

50

60

70

80

90

100

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area1 for inline arrangement of 11cross7exit

Area1 for inline 0, 11cross-7exit

Area 1 for inline 5, 11cross-7exit

Figure 110. Nu Vs Re (Area 1 for inline arrangement 11crossover holes-7exit holes)

85

20

30

40

50

60

70

80

90

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area2 for inline arrangement of 11cross7exit

Area2 for inline 0, 11cross-7exit

Area 2 for inline 5, 11cross-7exit

Figure 111. Nu Vs Re (Area 2 for inline arrangement 11crossover holes-7exit holes)

20

30

40

50

60

70

80

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area3 for inline arrangement of 11cross7exit

Area3 for inline 0, 11cross-7exit

Area3 for inline 5, 11cross-7exit

Figure 112. Nu Vs Re (Area 3 for inline arrangement 11crossover holes-7exit holes)

86

15

25

35

45

55

65

75

5000 10000 15000 20000 25000 30000 35000 40000

Nu

Re

Area4 for inline arrangement of 11cross7exit

Area4 for inline 0, 11cross-7exit

Area4 for inline 5, 11cross-7exit

Figure 113. Nu Vs Re (Area 4 for inline arrangement 11crossover holes-7exit holes)

Discussion of the figures above

For all cases, those Nusselt Numbers were plotted versus the jet Reynolds Numbers.

Three types of comparisons were made in the above figures:

Type1. For the same geometry, the average Nusselt numbers of all target areas

were compared.

Type2. For the same tilt angle and holes arrangement, the average Nusselt

numbers of all target areas at different numbers of exit blocked holes were

compared.

Type3. For the same holes arrangement and numbers of blocked exit holes, the

average Nusselt numbers of all target areas at different tilt angle were compared.

87

Through these comparisons, contributions of the tilt angle and holes arrangement to the

heat transfer efficiency were found and concluded.

Further details of these figures are:

Figure 22 through 37 show the Nusselt Number versus Reynolds Number at different

pressure increments (13, 26, 40, 54, 69, 80) for all 16 geometries. They show a

monotonic increase in Nusselt Number as Reynolds Number increases with

increasing the pressure. This is because with the same coolant, flow at a higher flow

rate has a higher convective effect.

Figure 38 through 53 show the type 1 comparison for all the 16 geometries. For the

same geometry, average Nusselt numbers of four areas were compared:

I. Figure38, Figure42, Figure46 and Figure50 show average Nusselt number versus

Reynolds number on all four areas for 11 crossover holes-12 exit holes cases where

the highest Nusselt Number at area1 and the lowest at area 4. Nusselt number at area2

is very close to area1 while Nusselt number at area3 is lower than area2 but higher

than area4.

II. Other figures show average Nusselt number versus Reynolds number on all four areas

for cases with blocked exit holes. From area1 to area4, Nusselt number decreases

monotonously. The highest Nusselt Number occurs at area1 and the lowest at area 4.

Figure 70 through 85 show the type 2 comparison for all the 16 geometries. For each

individual area, Nusselt numbers at the same tilt angle and holes arrangenment but

different number of exit holes were compared.

88

I. Figure 70 through 73 show comparison of inline arrangement and zero tilt angle case.

Details can be seen from the Table 2 below.

Geometry Number

of holes

Nu at

13psi

Nu at

26psi

Nu at

40psi

Nu at

54psi

Nu at

69psi

Nu at

80psi Remarks

Area1

11-7 98% 99% 95% 88% 90% 89% Truly inline 4 blocked

11-8 108% 108% 109% 109% 102% 102% Truly inline 3 blocked

11-9 116% 123% 120% 111% 106% 108% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area2

11-7 94% 88% 83% 79% 75% 74% Truly inline 4 blocked

11-8 92% 87% 92% 92% 90% 87% Truly inline 3 blocked

11-9 107% 109% 114% 109% 104% 106% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area3

11-7 77% 74% 75% 75% 67% 66% Truly inline 4 blocked

11-8 83% 78% 80% 78% 73% 73% Truly inline 3 blocked

11-9 88% 88% 91% 91% 86% 85% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area4

11-7 67% 65% 65% 62% 64% 60% Truly inline 4 blocked

11-8 73% 67% 70% 64% 65% 59% Truly inline 3 blocked

11-9 80% 82% 77% 74% 68% 69% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Table 2. Comparison of Average Nusselt numbers with the respective reference for inline

arrangement and zero tilt angle case

In Table 2, the average Nusselt numbers of each target area with different geometries at

different venturi pressures are compared with their respective reference values. The exact

results are shown in percentage. In general, the variation tendency of average Nusselt

numbers with respect to the number of blocked exit holes is shown in the figure below.

89

30

35

40

45

50

55

60

65

70

75

80

Nu

11-12 11-9 11-8 11-7

Inline arrangement, zero degree

Area1

Area 2

Area 3

Area 4

For area1, as the number of blocked exit holes increases, the Nusselt number first

increases and then decreases. 11crossover holes and 9 exit holes has the highest Nu

number while 11crossover holes and 7 exit holes has the lowest.

For area2, as the number of blocked exit holes increases, the Nusselt number first

increases and then decreases. 11crossover holes and 9 exit holes has the highest Nu

number while 11crossover holes and 7 exit holes has the lowest.

For area3, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area4, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

90

II. Figure 74 through 77 show comparison of inline arrangement and five tilt angle case.

Details can be seen from Table 3 below.

Geometry Number

of holes

Nu at

13psi

Nu at

26psi

Nu at

40psi

Nu at

54psi

Nu at

69psi

Nu at

80psi Remarks

Area1

11-7 80% 78% 84% 86% 86% 89% Truly inline 4 blocked

11-8 88% 91% 94% 94% 91% 97% Truly inline 3 blocked

11-9 87% 93% 97% 93% 90% 94% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area2

11-7 68% 63% 69% 71% 75% 73% Truly inline 4 blocked

11-8 74% 67% 75% 77% 79% 81% Truly inline 3 blocked

11-9 85% 84% 85% 84% 84% 85% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area3

11-7 62% 60% 62% 64% 64% 68% Truly inline 4 blocked

11-8 61% 60% 69% 72% 72% 76% Truly inline 3 blocked

11-9 73% 69% 70% 74% 75% 79% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area4

11-7 81% 74% 79% 76% 77% 78% Truly inline 4 blocked

11-8 83% 77% 82% 87% 85% 89% Truly inline 3 blocked

11-9 87% 83% 86% 91% 93% 95% Truly inline 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Table 3. Comparison of Average Nusselt numbers with the respective reference for inline

arrangement and five tilt angle case

In Table 3, the average Nusselt numbers of each target area with different geometries at

different venturi pressures are compared with their respective reference values. The exact

results are shown in percentage. In general, the variation tendency of average Nusselt

numbers with respect to the number of blocked exit holes is shown in the figure below.

91

40

45

50

55

60

65

70

75

80

85

90

Nu

11-12 11-9 11-8 11-7

Inline arrangement, five degree

Area1

Area 2

Area 3

Area 4

For area1, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area2, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area3, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area4, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

92

III. Figure 78 through 81 show comparison of staggered arrangement and zero tilt angle

case. Details can be seen from Table 4 below.

Geometry Number

of holes

Nu at

13psi

Nu at

26psi

Nu at

40psi

Nu at

54psi

Nu at

69psi

Nu at

80psi Remarks

Area1

11-8 100% 96% 94% 98% 98% 92% Truly staggered 4 blocked

11-9 104% 103% 101% 105% 106% 103% Truly staggered 3 blocked

11-10 111% 106% 108% 111% 111% 111% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area2

11-8 80% 81% 81% 84% 80% 75% Truly staggered 4 blocked

11-9 89% 86% 82% 87% 87% 85% Truly staggered 3 blocked

11-10 97% 96% 90% 98% 96% 96% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area3

11-8 74% 72% 72% 74% 73% 72% Truly staggered 4 blocked

11-9 80% 75% 75% 76% 79% 81% Truly staggered 3 blocked

11-10 85% 82% 85% 84% 82% 85% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area4

11-8 70% 70% 68% 68% 67% 68% Truly staggered 4 blocked

11-9 73% 72% 72% 71% 73% 80% Truly staggered 3 blocked

11-10 78% 75% 77% 76% 76% 82% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Table 4. Comparison of Average Nusselt numbers with the respective reference for

staggered arrangement and zero tilt angle case

In Table 4, the average Nusselt numbers of each target area with different geometries at

different venturi pressures are compared with their respective reference values. The exact

results are shown in percentage. In general, the variation tendency of average Nusselt

numbers with respect to the number of blocked exit holes is shown in the figure below.

93

30

35

40

45

50

55

60

65

70

75

80

Nu

11-12 11-9 11-8 11-7

Staggered arrangement, zero degree

Area1

Area 2

Area 3

Area 4

For area1, as the number of blocked exit holes increases, the Nusselt number first

increases and then decreases. 11crossover holes and 9 exit holes has the highest Nu

number while 11crossover holes and 7 exit holes has the lowest.

For area2, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area3, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area4, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

94

IV. Figure 82 through 85 show comparison of staggered arrangement and five tilt angle

case. Details can be seen from Table 5 below.

Geometry Number

of holes

Nu at

13psi

Nu at

26psi

Nu at

40psi

Nu at

54psi

Nu at

69psi

Nu at

80psi Remarks

Area1

11-8 86% 88% 87% 85% 91% 89% Truly staggered 4 blocked

11-9 98% 93% 91% 96% 98% 96% Truly staggered 3 blocked

11-10 116% 104% 105% 104% 105% 105% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area2

11-8 74% 73% 71% 73% 75% 78% Truly staggered 4 blocked

11-9 84% 80% 81% 83% 82% 81% Truly staggered 3 blocked

11-10 102% 92% 92% 95% 96% 98% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area3

11-8 75% 70% 68% 68% 71% 73% Truly staggered 4 blocked

11-9 89% 81% 77% 76% 74% 75% Truly staggered 3 blocked

11-10 98% 94% 86% 85% 83% 83% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Area4

11-8 72% 72% 68% 69% 68% 72% Truly staggered 4 blocked

11-9 86% 83% 79% 78% 74% 73% Truly staggered 3 blocked

11-10 100% 93% 87% 88% 84% 84% Truly staggered 2 blocked

11-12 100% 100% 100% 100% 100% 100% Reference

Table 5. Comparison of Average Nusselt numbers with the respective reference for

staggered arrangement and five tilt angle case

In Table 5, the average Nusselt numbers of each target area with different geometries at

different venturi pressures are compared with their respective reference values. The exact

results are shown in percentage. In general, the variation tendency of average Nusselt

numbers with respect to the number of blocked exit holes is shown in the figure below.

95

40

45

50

55

60

65

70

75

80

85

90

Nu

11-12 11-9 11-8 11-7

Staggered arrangement, five degree

Area1

Area 2

Area 3

Area 4

For area1, as the number of blocked exit holes increases, the Nusselt number first

increases and then decreases. 11crossover holes and 9 exit holes has the highest Nu

number while 11crossover holes and 7 exit holes has the lowest.

For area2, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area3, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

For area4, as the number of blocked exit holes increases, the Nusselt number decreases.

11crossover holes and 12 exit holes has the highest Nu number while 11crossover holes

and 7 exit holes has the lowest.

96

Figure 86 through 89 show the comparison between inline and staggered

arrangements for 11 crossover holes and 12 exit holes at zero and five tilt angles for

areas 1 through 4 consecutively. The conclusion is that the Nusselt Number at five tilt

angle is higher than that at zero tilt angle. For the same tilt angle, inline arrangement

and staggered arrangement have almost the same heat transfer coefficients which

means staggered or inline arrangement did not play an important role in the heat

transfer coefficients.

Figure 90 through 113 show the comparison between zero and five tilt angles for each

specific area and arrangement.

I. For inline arrangement, Nusselt Numbers at five degree tilt angles are

higher than those at zero degree tilt angles.

II. For staggered arrangement, Nusselt Numbers at five degree tilt angles are

higher than those at zero degree tilt angles.

.

97

Conclusion:

An experiment investigation was conducted to determine the effect of the number of

blocked exit holes on impinging heat transfer coefficient in a trailing-edge cooling

channel. This experiment simulated the cooling flow in a trailing edge cooling cavity of a

turbine airfoil for a typical gas turbine engine. Total 16 cases were tested in this

experiment, and for all cases, the experiments were set up for closed bleed valve. The

conclusions of this experimental study are listed below:

1. The Nusselt number increased monotonically as the Reynolds number increased

2. The staggered or inline arrangement did not play an important role in the heat

transfer coefficients.

3. For the same geometry, The Nusselt number of five tilt angle was higher than that

of zero tilt angle for both staggered and inline arrangement cases.

4. For staggered arrangement, the highest Nusselt numbers were found in the area

two holes away from the nearest blocked exit hole. Thus as the number of blocked

exit holes increased, the Nusselt number of area1 increased first and then

decreased. The Nusselt numbers of other three areas decreased monotonically.

5. For inline arrangement, conclusions are different between zero tilt angle and five

tilt angle. With zero tilt angle, the Nusselt numbers of area1 and area2 both

increased first and then decreased as the number of blocked holes increased.

98

While with five tilt angle, Nusselt numbers of all the four areas decreased

monotonically.

As to get more accurate conclusions, I suggest in the next experiment, more than four

areas should be focused and tested especially for inline cases.

99

References

[1] Taslim, M.E., Nicolas, G.J., “An Experimental and Numerical Investigation of Jet

Impingement on Ribs in an Airfoil Trailing-Edge Cooling Channel,” ISROMAC 12-

2008-20238, pp. 1-8.

[2] Taslim, M.E., Li, T. and Spring, S.D., “Measurements of Heat Transfer Coefficients

in Rib-Roughened Trailing-Edge Cavities with Crossover Jets,” ASME Paper No. 98-

GT-435, 1998.

[3] Taslim, M.E., and Nongsaeng, A., “Experimental and Numerical Cross-Over Jet

Impingement in an Airfoil Trailing-Edge Cooling Channel,” 2011.

[4] Kline, S.J. and McClintock, F. A., “Calculating Uncertainty in Single Sample

Experiments,” Mechanical Engineering, January 1953, pp. 3-8.

[5] Azar, K., Benson, J.R., Manno, V.P., “Liquid crystal imaging for temperature

measurement of electronic devices” Semiconductor Thermal Measurement and

Management Symposium, Vol.12-14, February 1991, pp. 23-33.

[6] Kreith Frank., “The CRC handbook of thermal engineering,” 2000.

A -1

Appendix A: Log sheets for each experiment

The log sheets are displayed in the following order: Cold test and Heat transfer tests (which is

tested under 6 pressures 13, 26, 40, 54, 69, 80psi)

The order of theses log sheets are:

Geomtry1: 11crossover holes-12 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Geomtry2: 11crossover holes-9 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Geomtry3: 11crossover holes-8exit holes, inline arrangement, 0 degree tilt angle, no bleed

Geomtry4: 11crossover holes-7 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Geomtry5: 11crossover holes-12 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Geomtry6: 11crossover holes-9exit holes, inline arrangement, 5 degree tilt angle, no bleed

Geomtry7: 11crossover holes-8 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Geomtry8: 11crossover holes-7 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Geomtry9: 11crossover holes-12 exit holes, staggered arrangement, 0 degree tilt angle, no

bleed

Geomtry10: 11crossover holes-10 exit holes, staggered arrangement, 0 degree tilt angle, no

bleed

Geomtry11: 11crossover holes-9 exit holes, staggered arrangement, 0 degree tilt angle, no

bleed

Geomtry12: 11crossover holes-8 exit holes, staggered arrangement, 0 degree tilt angle, no

bleed

A -2

Geomtry13: 11crossover holes-12 exit holes, staggered arrangement, 5 degree tilt angle, no

bleed

Geomtry14: 11crossover holes-10 exit holes, staggered arrangement, 5 degree tilt angle, no

bleed

Geomtry15: 11crossover holes-9 exit holes, staggered arrangement, 5 degree tilt angle, no

bleed

Geomtry16: 11crossover holes-8 exit holes, staggered arrangement, 5 degree tilt angle, no

bleed

A -3

11crossover holes-12 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---12 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 40 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 73.6 73.3 73.3 74.5 0.201 0.183 0.188 0.195 0.092 0.087 water 30.07 0.024 73.2 0

10 73.5 73 73.1 74.5 0.333 0.307 0.306 0.317 0.168 0.155 water 30.07 0.017 72.9 0

15 73.6 73 73.1 74.5 0.489 0.454 0.464 0.47 0.265 0.237 water 30.07 0.017 73 0

20 73.6 72.8 72.9 74.5 0.667 0.621 0.641 0.649 0.372 0.339 water 30.07 0.021 72.8 0

25 69.5 70.1 70.4 73.8 0.883 0.825 0.846 0.853 0.477 0.454 wtaer 30.23 0.02 70.1 0

30 69.6 70.2 70.4 73.8 2.71 2.53 2.6 2.65 1.5 1.41 orange 30.23 0.05 70.1 0

40 69.8 69.8 70 73.8 4.02 3.77 3.86 3.89 2.32 2.12 orange 30.23 0.1 69.7 0

50 69.5 70.1 70.3 73.8 5.56 5.19 5.32 5.39 3.25 2.93 orange 30.23 0.17 69.8 0

60 69.8 69.9 70.1 73.8 7.15 6.82 7.02 7.11 4.29 3.89 orange 30.23 0.2 69.8 0

70 73.5 72.2 72.4 74.6 9.29 8.3 8.93 8.99 5.45 4.99 orange 30.21 0.2 74.6 0

80 76.9 74.5 74.7 73.6 11.55 10.74 10.99 11.18 6.78 6.19 orange 30.22 0.59 74.4 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

Xiao Huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.1 71.8 72.0 71.8 73.7 80.4 70.5 0 0 20.04 0.4659 20.04 0.4641 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

2a,b,c 69.2 71.7 72.0 71.8 73.6 82.4 70.5 0 0 20.66 0.4802 20.73 0.4797 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

3a,b,c 68.8 71.5 71.9 71.6 73.5 83.6 70.5 0 0 21.25 0.4937 21.19 0.4905 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

4a,b,c 68.4 71.5 71.8 71.6 73.5 84.8 70.5 0 0 21.92 0.5092 21.76 0.5033 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

5a,b,c 68.2 71.4 71.7 71.5 73.4 85.8 70.5 0 0 22.53 0.5236 22.50 0.5207 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

6a,b,c 67.9 71.2 71.5 71.3 73.3 86.6 70.5 0 0 23.13 0.5374 23.07 0.5338 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

7a,b,c 68.0 71.1 71.4 71.1 73.2 87.5 70.5 0 0 23.64 0.5484 23.62 0.5460 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

8a,b,c 68.0 71.0 71.3 71.1 73.2 88.3 70.5 0 0 24.30 0.5644 24.35 0.5632 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

9a,b,c 67.8 71.0 71.4 71.1 73.2 89.5 70.5 0 0 24.86 0.5775 24.84 0.5745 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

10a,b,c 68.1 70.9 71.2 71.0 73.1 90.2 70.5 0 0 25.47 0.5917 25.48 0.5893 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

11a,b,c 68.1 70.8 71.2 70.9 73.0 90.9 70.5 0 0 26.03 0.6045 26.02 0.6017 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

12a,b,c 67.8 70.8 71.2 71.0 73.1 92.1 70.5 0 0 26.64 0.6187 26.63 0.6157 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

13a,b,c 67.8 70.8 71.2 71.0 73.0 93.2 70.5 0 0 27.22 0.6321 27.27 0.6306 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

14a,b,c 67.9 70.8 71.1 70.9 72.9 94.2 70.5 0 0 27.79 0.6454 27.80 0.6427 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

15a,b,c 68.7 71.0 71.2 71.0 73.0 95.2 70.5 0 0 28.38 0.6590 28.39 0.6562 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

16a,b,c 68.2 70.9 71.2 71.0 72.9 96.5 70.5 0 0 29.05 0.6747 29.03 0.6706 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

17a,b,c 68.6 71.0 71.4 71.2 73.0 97.7 70.5 0 0 29.58 0.6865 29.69 0.6855 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

18a,b,c 68.6 71.0 71.3 71.1 73.0 98.6 70.5 0 0 30.19 0.7005 30.26 0.6989 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

19a,b,c 68.7 71.1 71.5 71.1 73.1 99.8 70.5 0 0 30.82 0.7150 30.90 0.7136 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

20a,b,c 68.8 71.2 71.5 71.3 73.0 101.2 70.5 0 0 31.46 0.7310 31.48 0.7281 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

21a,b,c 68.7 71.1 71.4 71.1 73.0 102.7 70.5 0 0 32.28 0.7484 32.29 0.7468 2 0.431 0.396 0.404 0.416 0.249 0.211 0.014 30.05

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -4

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.2 72.8 72.9 72.7 73.4 79.8 74.5 0 0 21.14 0.4913 21.12 0.4891 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

2a,b,c 73.6 72.8 72.9 72.8 73.4 81.2 74.5 0 0 21.79 0.5062 21.84 0.5054 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

3a,b,c 73.6 73.0 73.1 73.0 73.5 82.3 74.5 0 0 22.65 0.5262 22.58 0.5225 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

4a,b,c 73.5 73.0 73.1 72.9 73.4 83.4 74.5 0 0 23.49 0.5457 23.42 0.5419 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

5a,b,c 73.6 73.3 73.3 73.2 73.6 84.6 74.5 0 0 24.20 0.5620 24.20 0.5599 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

6a,b,c 74.2 73.3 73.4 73.2 73.7 85.4 74.5 0 0 24.94 0.5793 24.91 0.5768 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

7a,b,c 73.7 73.4 73.6 73.3 73.9 86.7 74.5 0 0 25.63 0.5955 25.70 0.5949 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

8a,b,c 73.6 73.5 73.7 73.5 74.0 87.7 74.5 0 0 26.36 0.6122 26.38 0.6105 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

9a,b,c 73.3 73.7 73.8 73.6 74.1 88.8 74.5 0 0 27.01 0.6271 27.09 0.6266 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

10a,b,c 73.4 73.7 73.8 73.6 74.1 89.7 74.5 0 0 27.78 0.6447 27.70 0.6407 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

11a,b,c 73.6 73.7 73.8 73.5 74.2 90.5 74.5 0 0 28.45 0.6605 28.43 0.6573 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

12a,b,c 72.9 73.5 73.6 73.4 74.2 91.3 74.5 0 0 29.11 0.6758 29.08 0.6726 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

13a,b,c 72.9 73.4 73.6 73.3 74.2 92.4 74.5 0 0 29.72 0.6900 29.63 0.6853 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

14a,b,c 73.0 73.3 73.5 73.3 74.2 92.9 74.5 0 0 30.37 0.7048 30.41 0.7031 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

15a,b,c 72.2 73.3 73.4 73.2 74.1 94.1 74.5 0 0 31.14 0.7230 31.20 0.7214 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

16a,b,c 72.4 73.2 73.4 73.1 74.2 95.4 74.5 0 0 31.94 0.7414 31.91 0.7374 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

17a,b,c 72.3 73.0 73.2 73.0 74.0 96.1 74.5 0 0 32.73 0.7591 32.66 0.7548 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

18a,b,c 71.4 73.0 73.2 72.8 74.1 97.3 74.5 0 0 33.51 0.7774 33.52 0.7746 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

19a,b,c 71.3 72.7 73.0 72.8 73.9 98.7 74.5 0 0 34.23 0.7944 34.36 0.7941 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

20a,b,c 71.1 72.7 72.9 72.7 73.9 99.8 74.5 0 0 35.03 0.8119 35.05 0.8097 2 0.924 0.855 0.874 0.882 0.516 0.473 0.033 30.07

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.8 69.8 70.0 69.7 71.1 79.1 73.8 0 0 23.98 0.5574 24.08 0.5576 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

2a,b,c 69.8 69.9 70.1 69.8 71.1 80.2 73.8 0 0 24.97 0.5803 24.96 0.5780 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

3a,b,c 69.5 70.1 70.3 70.0 71.3 81.3 73.8 0 0 26.00 0.6042 25.96 0.6011 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

4a,b,c 69.6 70.2 70.4 70.1 71.4 82.3 73.8 0 0 27.03 0.6272 27.02 0.6253 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

5a,b,c 69.5 70.1 70.4 70.1 71.4 83.7 73.8 0 0 28.04 0.6515 28.08 0.6500 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

6a,b,c 69.7 70.3 70.5 70.2 71.5 84.2 73.8 0 0 29.06 0.6749 28.96 0.6703 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

7a,b,c 69.4 70.3 70.5 70.2 71.5 85.6 73.8 0 0 30.08 0.6987 30.09 0.6962 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

8a,b,c 68.9 70.0 70.3 70.0 71.4 86.6 73.8 0 0 31.00 0.7199 31.08 0.7192 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

9a,b,c 68.9 69.9 70.2 69.8 71.4 87.7 73.8 0 0 32.03 0.7433 31.94 0.7388 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

10a,b,c 69.1 69.8 70.1 69.8 71.3 89.0 73.8 0 0 32.98 0.7658 33.08 0.7652 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

11a,b,c 69.0 69.6 69.9 69.5 71.2 90.1 73.8 0 0 33.96 0.7883 34.18 0.7903 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

12a,b,c 69.1 69.6 69.9 69.5 71.2 91.2 73.8 0 0 35.02 0.8130 35.05 0.8103 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

13a,b,c 69.0 69.5 69.8 69.5 71.2 92.6 73.8 0 0 36.06 0.8369 36.09 0.8342 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

14a,b,c 68.0 69.2 69.6 69.2 71.0 93.6 73.8 0 0 36.99 0.8583 37.02 0.8557 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

15a,b,c 68.3 69.2 69.6 69.2 71.0 94.7 73.8 0 0 38.05 0.8828 38.02 0.8785 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

16a,b,c 68.8 69.2 69.6 69.2 70.9 95.9 73.8 0 0 39.07 0.9063 39.05 0.9022 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

17a,b,c 68.4 69.3 69.6 69.2 70.9 97.0 73.8 0 0 40.03 0.9285 40.09 0.9258 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

18a,b,c 68.0 69.3 69.5 69.2 71.0 98.7 73.8 0 0 41.06 0.9520 41.06 0.9481 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

19a,b,c 67.7 69.2 69.6 69.2 71.0 100.2 73.8 0 0 42.11 0.9760 42.02 0.9701 2 4.020 3.770 3.860 3.890 2.320 2.120 0.100 30.23

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -5

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.1 72.2 72.4 72.1 72.7 79.7 74.8 0 0 24.54 0.5704 24.55 0.5686 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

2a,b,c 72.8 72.2 72.4 72.1 72.7 80.7 74.8 0 0 25.64 0.5959 25.58 0.5922 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

3a,b,c 73.6 72.4 72.5 72.3 72.9 81.7 74.8 0 0 26.70 0.6204 26.70 0.6183 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

4a,b,c 73.2 72.3 72.4 72.2 72.8 82.6 74.8 0 0 27.29 0.6456 27.81 0.6439 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

5a,b,c 72.4 72.2 72.4 72.1 72.9 83.6 74.8 0 0 28.90 0.6707 28.86 0.6682 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

6a,b,c 72.3 72.2 72.4 72.1 72.9 84.3 74.8 0 0 30.01 0.6972 29.98 0.6938 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

7a,b,c 72.3 72.0 72.2 71.9 72.8 85.3 74.8 0 0 31.17 0.7239 31.16 0.7210 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

8a,b,c 72.1 71.9 72.1 71.8 72.9 86.1 74.8 0 0 32.31 0.7503 32.23 0.7461 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

9a,b,c 71.9 71.9 72.1 71.8 72.8 87.3 74.8 0 0 33.32 0.7735 33.30 0.7703 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

10a,b,c 71.8 71.6 71.8 71.5 72.6 88.1 74.8 0 0 34.41 0.7990 34.43 0.7964 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

11a,b,c 71.2 71.4 71.7 71.3 72.5 89.0 74.8 0 0 35.56 0.8255 35.58 0.8227 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

12a,b,c 71.4 71.3 71.6 71.3 72.5 90.1 74.8 0 0 36.60 0.8499 36.64 0.8471 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

13a,b,c 71.3 71.3 71.5 71.2 72.4 91.1 74.8 0 0 37.78 0.8759 37.69 0.8714 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

14a,b,c 70.7 71.0 71.3 70.9 72.2 92.2 74.8 0 0 38.93 0.9037 38.83 0.8976 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

15a,b,c 71.0 70.9 71.1 70.8 72.1 93.0 74.8 0 0 39.96 0.9270 40.02 0.9248 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

16a,b,c 70.6 70.8 71.1 70.8 72.1 94.2 74.8 0 0 41.06 0.9522 41.02 0.9477 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

17a,b,c 70.5 70.7 71.0 70.7 72.0 95.4 74.8 0 0 42.11 0.9766 42.19 0.9746 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

18a,b,c 70.3 70.6 71.0 70.6 72.0 96.5 74.8 0 0 43.19 1.0012 43.30 0.9992 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

19a,b,c 70.2 70.6 70.9 70.6 72.0 98.1 74.8 0 0 44.31 1.0273 44.34 1.0238 2 6.290 5.910 6.020 6.090 3.690 3.290 0.170 30.21

20a,b,c 70.3 70.6 70.9 70.6 71.9 98.9 74.8 0 0 45.45 1.0528 45.45 1.0490 2 6.29 5.91 6.02 6.09 3.69 3.29 0.17 30.21

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.5 72.2 74.3 72.1 72.9 79.7 74.6 0 0 25.90 0.6019 25.86 0.5991 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

2a,b,c 73.1 72.4 74.2 72.3 73.1 80.4 74.6 0 0 27.02 0.6278 26.99 0.6250 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

3a,b,c 73.7 72.3 73.9 72.2 73.1 81.2 74.6 0 0 28.23 0.6561 28.32 0.6558 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

4a,b,c 72.5 72.1 73.7 72.1 73.1 82.2 74.6 0 0 29.45 0.6842 29.50 0.6829 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

5a,b,c 73.1 72.2 73.6 72.1 73.1 82.9 74.6 0 0 30.68 0.7126 30.54 0.7071 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

6a,b,c 73.1 72.0 73.3 71.9 73.0 83.6 74.6 0 0 31.86 0.7398 31.82 0.7367 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

7a,b,c 72.7 71.6 72.9 71.0 72.8 84.5 74.6 0 0 33.01 0.7667 33.06 0.7651 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

8a,b,c 72.3 71.5 72.8 71.4 72.7 85.3 74.6 0 0 34.35 0.7977 34.32 0.7941 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

9a,b,c 72.1 71.4 72.7 71.3 72.6 85.9 74.6 0 0 35.38 0.8215 35.39 0.8187 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

10a,b,c 72.0 71.1 72.6 71.0 72.4 87.1 74.6 0 0 36.72 0.8523 36.66 0.8476 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

11a,b,c 71.6 71.0 72.6 71.0 72.3 88.0 74.6 0 0 37.88 0.8791 37.87 0.8760 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

12a,b,c 71.2 71.0 72.7 70.9 72.2 88.6 74.6 0 0 39.07 0.9068 39.05 0.9031 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

13a,b,c 71.5 70.9 72.9 70.8 72.2 89.5 74.6 0 0 40.20 0.9327 40.17 0.9288 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

14a,b,c 71.5 70.8 73.0 70.8 72.1 90.8 74.6 0 0 41.43 0.9611 41.51 0.9594 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

15a,b,c 71.3 70.9 73.1 70.8 72.1 91.9 74.6 0 0 42.66 0.9894 42.69 0.9862 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

16a,b,c 71.7 70.8 73.1 70.8 72.0 93.1 74.6 0 0 43.77 1.0149 43.69 1.0093 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

17a,b,c 72.1 70.9 73.2 70.9 72.0 94.3 74.6 0 0 45.07 1.0447 45.07 1.0413 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

18a,b,c 72.3 70.9 73.4 70.9 72.0 95.4 74.6 0 0 46.33 1.0736 46.16 1.0658 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

19a,b,c 71.9 70.9 73.4 70.9 72.0 96.1 74.6 0 0 47.46 1.0994 47.41 1.0940 orange 9.290 8.700 8.930 8.990 5.450 4.990 0.200 30.21

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -6

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/30/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.9 74.5 74.7 74.4 75.0 80.4 73.6 0 0 25.56 0.5942 25.62 0.5932 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

2a,b,c 75.5 74.4 74.6 74.3 74.9 81.2 73.6 0 0 27.03 0.6283 27.07 0.6268 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

3a,b,c 75.9 74.2 74.4 74.1 74.8 82.0 73.6 0 0 28.49 0.6619 28.55 0.6613 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

4a,b,c 75.6 74.0 74.1 73.8 74.7 82.7 73.6 0 0 30.06 0.6983 30.03 0.6954 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

5a,b,c 75.0 73.7 73.9 73.6 74.5 83.6 73.6 0 0 31.48 0.7313 31.41 0.7271 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

6a,b,c 75.2 73.3 73.6 73.3 74.3 84.5 73.6 0 0 32.94 0.7651 33.00 0.7631 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

7a,b,c 74.1 73.2 73.4 73.1 74.2 85.3 73.6 0 0 34.59 0.8033 34.61 0.8009 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

8a,b,c 74.6 73.1 73.3 73.0 74.1 86.3 73.6 0 0 36.01 0.8363 36.08 0.8348 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

9a,b,c 74.3 72.9 73.2 72.9 73.9 87.2 73.6 0 0 37.44 0.8691 37.40 0.8650 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

10a,b,c 73.9 72.8 73.0 72.8 73.8 87.8 73.6 0 0 38.44 0.8924 38.41 0.8883 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

11a,b,c 73.8 72.6 72.8 72.6 73.7 89.0 73.6 0 0 39.49 0.9159 39.47 0.9130 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

12a,b,c 73.7 72.4 72.6 72.4 73.5 89.3 73.6 0 0 40.52 0.9403 40.50 0.9364 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

13a,b,c 73.3 72.1 72.4 72.1 73.3 90.2 73.6 0 0 41.43 0.9609 41.56 0.9610 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

14a,b,c 72.5 72.0 72.3 72.0 73.2 90.9 73.6 0 0 42.59 0.9874 42.50 0.9822 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

15a,b,c 72.6 71.9 72.2 71.9 73.1 91.8 73.6 0 0 43.53 1.0094 43.51 1.0056 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

16a,b,c 72.6 71.9 72.1 71.9 73.1 92.6 73.6 0 0 44.52 1.0324 44.51 1.0285 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

17a,b,c 73.4 71.9 72.2 72.0 73.1 93.5 73.6 0 0 45.58 1.0567 45.50 1.0505 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

18a,b,c 73.4 71.9 72.1 71.9 73.0 94.6 73.6 0 0 46.46 1.0763 46.53 1.0739 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

19a,b,c 73.5 71.8 72.1 71.8 72.9 95.1 73.6 0 0 47.54 1.1019 47.51 1.0958 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

20a,b,c 73.3 71.8 72.1 71.8 72.9 95.5 73.6 0 0 48.63 1.1267 48.69 1.1234 orange 11.55 10.74 10.99 11.18 6.78 6.19 0.21 30.22

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -7

11crossover holes-9 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---9 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 30 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 73.3 73.2 73.4 70.0 0.324 0.307 0.309 0.321 0.205 0.246 water 30.02 0.017 73.4 0

10 73.2 73.5 73.7 70.0 0.512 0.488 0.493 0.502 0.336 0.397 water 30.02 0.027 73.1 0

15 74.1 73.5 73.6 70.0 0.764 0.725 0.738 0.740 0.503 0.380 water 30.02 0.039 73.3 0

20 73.2 73.5 73.7 70.0 2.490 2.390 2.390 2.390 1.700 1.990 water 30.02 0.11 73.5 0

25 74.1 73.8 73.9 70.0 3.380 3.190 3.190 3.210 2.300 2.600 orange 29.99 0.25 74.1 0

30 75.6 74.5 74.7 72.6 4.190 3.990 3.990 4.070 2.880 3.290 orange 29.99 0.200 74.3 0

40 76.0 74.4 74.6 72.6 6.420 6.170 6.270 6.290 4.490 5.180 orange 29.99 0.31 74.4 0

50 76.2 74.6 74.7 72.6 8.590 8.180 8.320 8.490 5.960 6.890 orange 29.99 0.39 74.4 0

60 76.2 74.6 74.8 72.6 11.280 10.790 10.990 10.980 7.890 9.090 orange 29.99 0.53 74.5 0

70 76.5 74.6 74.8 72.6 14.490 13.860 14.110 14.180 10.090 11.660 orange 29.99 0.73 74.6 0

80 73.4 68.9 69.2 73.6 17.610 16.910 17.110 17.210 12.210 14.300 orange 30.01 0.78 69 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.3 73.5 73.7 73.5 74.4 78.8 72.2 0 0 18.52 0.4304 18.85 0.4364 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

2a,b,c 72.6 73.6 73.8 73.6 74.4 80.1 72.2 0 0 19.75 0.4590 19.65 0.4547 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

3a,b,c 72.4 73.5 73.6 73.4 74.4 80.8 72.2 0 0 20.55 0.4775 20.57 0.4759 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

4a,b,c 73.0 73.4 73.6 73.3 74.4 81.7 72.2 0 0 21.30 0.4950 21.33 0.4937 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

5a,b,c 72.3 73.3 73.5 73.3 74.3 82.5 72.2 0 0 22.15 0.5145 22.24 0.5147 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

6a,b,c 72.9 73.2 73.4 73.2 74.3 83.3 72.2 0 0 23.00 0.5344 23.07 0.5338 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

7a,b,c 72.6 73.1 73.2 73.1 74.2 83.9 72.2 0 0 23.81 0.5532 23.81 0.5510 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

8a,b,c 72.4 72.9 73.2 73.0 74.2 84.6 72.2 0 0 24.66 0.5730 24.65 0.5705 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

9a,b,c 71.9 73.0 73.2 73.0 74.1 85.5 72.2 0 0 25.42 0.5908 25.44 0.5888 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

10a,b,c 72.6 73.0 73.2 73.0 74.1 86.1 72.2 0 0 26.20 0.6083 26.13 0.6042 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

11a,b,c 72.7 73.0 73.2 73.0 74.1 87.2 72.2 0 0 27.05 0.6282 27.02 0.6249 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

12a,b,c 71.9 73.0 73.2 73.1 74.1 87.8 72.2 0 0 27.98 0.6497 27.99 0.6472 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

13a,b,c 72.1 73.0 73.2 73.1 74.1 88.8 72.2 0 0 28.92 0.6713 28.86 0.6670 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

14a,b,c 72.3 73.1 73.3 73.1 74.1 89.8 72.2 0 0 29.74 0.6903 29.69 0.6863 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

15a,b,c 72.6 73.2 73.4 73.3 74.1 91.0 72.2 0 0 30.52 0.7084 30.40 0.7025 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

16a,b,c 73.1 73.2 73.4 73.3 74.2 92.1 72.2 0 0 31.28 0.7258 31.29 0.7229 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

17a,b,c 72.8 73.3 73.5 73.3 74.2 93.2 72.2 0 0 32.01 0.7428 31.99 0.7389 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

18a,b,c 73.2 73.3 73.5 73.3 74.2 94.3 72.2 0 0 32.79 0.7605 32.83 0.7584 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

19a,b,c 73.2 73.3 73.5 73.3 74.2 95.4 72.2 0 0 33.67 0.7810 33.61 0.7762 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

20a,b,c 72.9 73.3 73.5 73.3 74.2 96.5 72.2 0 0 34.43 0.7984 34.46 0.7956 orange 0.696 0.655 0.661 0.669 0.456 0.534 0.029 30.05

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -8

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.1 73.8 73.9 73.8 74.3 78.1 70.0 0 0 20.08 0.4668 20.19 0.4674 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

2a,b,c 73.2 73.5 73.7 73.5 74.2 78.9 70.0 0 0 21.03 0.4888 20.98 0.4858 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

3a,b,c 74.1 73.5 73.6 73.4 74.2 79.6 70.0 0 0 22.06 0.5126 21.89 0.5058 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

4a,b,c 73.3 73.3 73.5 73.3 74.1 80.3 70.0 0 0 23.10 0.5367 23.10 0.5345 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

5a,b,c 73.3 73.2 73.4 73.1 74.0 80.9 70.0 0 0 24.13 0.5607 24.20 0.5602 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

6a,b,c 73.3 73.3 73.5 73.4 74.1 81.6 70.0 0 0 25.10 0.5830 25.30 0.5857 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

7a,b,c 74.0 73.4 73.6 73.4 74.1 82.3 70.0 0 0 26.07 0.6056 26.10 0.6038 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

8a,b,c 74.3 73.4 73.6 73.4 74.1 83.1 70.0 0 0 27.06 0.6279 27.12 0.6276 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

9a,b,c 73.9 73.4 73.6 73.4 74.1 83.8 70.0 0 0 28.04 0.6511 28.09 0.6499 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

10a,b,c 73.7 73.4 73.6 73.4 74.1 84.5 70.0 0 0 28.99 0.6733 29.04 0.6718 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

11a,b,c 73.6 73.5 73.7 73.5 74.1 85.6 70.0 0 0 30.03 0.6975 30.04 0.6947 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

12a,b,c 74.7 73.6 73.8 73.6 74.2 86.4 70.0 0 0 31.25 0.7255 31.04 0.7175 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

13a,b,c 74.1 73.7 73.9 73.7 74.2 87.5 70.0 0 0 32.09 0.7447 32.21 0.7452 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

14a,b,c 74.8 73.7 73.9 73.7 74.3 88.4 70.0 0 0 33.04 0.7667 33.07 0.7643 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

15a,b,c 74.3 73.7 73.9 73.7 74.3 89.3 70.0 0 0 34.13 0.7918 34.22 0.7909 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

16a,b,c 74.8 73.7 73.9 73.7 74.3 90.5 70.0 0 0 35.13 0.8151 35.41 0.8183 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

17a,b,c 74.3 73.9 74.1 73.8 74.4 91.6 70.0 0 0 35.99 0.8350 36.11 0.8341 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

18a,b,c 74.8 73.8 74.0 73.8 74.4 92.6 70.0 0 0 37.02 0.8557 37.26 0.8604 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

19a,b,c 74.3 73.8 74.0 73.8 74.4 93.7 70.0 0 0 38.15 0.8845 38.30 0.8848 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

20a,b,c 74.4 73.6 73.8 73.5 74.3 94.5 70.0 0 0 39.06 0.9055 39.03 0.9012 orange 3.49 3.39 3.38 3.39 2.39 2.79 0.2 30.02

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.0 74.4 74.6 74.4 74.9 78.9 72.6 0 0 22.20 0.5159 22.11 0.5120 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

2a,b,c 76.5 74.6 74.8 74.6 75.0 79.7 72.6 0 0 23.19 0.5388 23.17 0.5368 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

3a,b,c 76.2 74.6 74.8 74.6 74.9 80.3 72.6 0 0 24.34 0.5657 24.36 0.5638 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

4a,b,c 76.2 74.6 74.7 74.5 75.0 80.9 72.6 0 0 25.39 0.5899 25.42 0.5884 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

5a,b,c 75.6 74.5 74.7 74.4 74.9 81.4 72.6 0 0 26.52 0.6161 26.57 0.6147 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

6a,b,c 74.9 74.5 74.6 74.3 74.9 82.0 72.6 0 0 27.63 0.6419 27.61 0.6388 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

7a,b,c 74.8 74.2 74.4 74.1 74.8 82.5 72.6 0 0 28.70 0.6665 28.70 0.6643 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

8a,b,c 75.3 74.1 74.3 74.0 74.7 83.0 72.6 0 0 29.82 0.6926 29.80 0.6894 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

9a,b,c 75.0 73.9 74.1 73.8 74.6 83.7 72.6 0 0 31.00 0.7199 30.98 0.7167 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

10a,b,c 74.5 73.7 73.9 73.6 74.4 84.3 72.6 0 0 31.99 0.7427 32.09 0.7420 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

11a,b,c 74.0 73.4 73.7 73.4 74.3 85.0 72.6 0 0 33.17 0.7700 33.26 0.7693 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

12a,b,c 73.8 73.3 73.6 73.2 74.2 85.5 72.6 0 0 34.30 0.7961 34.36 0.7944 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

13a,b,c 73.6 73.3 73.5 73.2 74.2 86.4 72.6 0 0 35.52 0.8250 35.51 0.8210 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

14a,b,c 74.3 73.3 73.5 73.3 74.2 87.2 72.6 0 0 36.59 0.8490 36.66 0.8475 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

15a,b,c 73.9 73.3 73.6 73.3 74.1 87.7 72.6 0 0 37.73 0.8752 37.67 0.8706 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

16a,b,c 73.8 73.6 73.8 73.6 74.2 88.9 72.6 0 0 38.78 0.8995 38.76 0.8956 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

17a,b,c 74.4 73.6 73.8 73.6 74.3 89.7 72.6 0 0 39.84 0.9237 39.83 0.9200 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

18a,b,c 74.0 73.6 73.8 73.6 74.3 90.5 72.6 0 0 41.04 0.9512 41.00 0.9470 orange 6.42 6.17 6.27 6.29 4.49 5.18 0.31 29.99

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -9

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.8 74.4 74.6 74.4 74.7 78.2 74.0 0 0 23.18 0.5388 23.15 0.5362 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

2a,b,c 76.0 74.5 74.6 74.4 74.7 78.9 74.0 0 0 24.31 0.5648 24.37 0.5642 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

3a,b,c 76.1 74.5 74.6 74.4 74.8 79.5 74.0 0 0 25.54 0.5937 25.54 0.5914 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

4a,b,c 76.1 74.4 74.6 74.4 74.7 80.0 74.0 0 0 26.71 0.6205 26.69 0.6178 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

5a,b,c 75.2 74.3 74.5 74.3 74.7 80.5 74.0 0 0 27.97 0.6498 27.94 0.6468 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

6a,b,c 75.5 74.4 74.5 74.2 74.8 81.2 74.0 0 0 29.15 0.6773 29.14 0.6744 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

7a,b,c 75.0 74.3 74.5 74.2 74.8 81.8 74.0 0 0 30.30 0.7036 30.27 0.7005 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

8a,b,c 74.9 74.2 74.4 74.1 74.7 82.3 74.0 0 0 31.54 0.7323 31.57 0.7306 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

9a,b,c 75.1 74.0 74.2 74.0 74.7 82.9 74.0 0 0 32.72 0.7598 32.72 0.7570 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

10a,b,c 74.2 73.9 74.1 73.9 74.7 83.5 74.0 0 0 33.96 0.7884 33.94 0.7852 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

11a,b,c 74.9 73.7 73.9 73.7 74.6 84.2 74.0 0 0 35.13 0.8155 35.01 0.8095 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

12a,b,c 74.3 73.4 73.6 73.4 74.4 84.7 74.0 0 0 36.27 0.8419 36.21 0.8370 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

13a,b,c 73.6 73.2 73.5 73.1 74.2 85.1 74.0 0 0 37.48 0.8690 37.41 0.8651 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

14a,b,c 73.8 72.9 73.1 72.8 74.0 85.8 74.0 0 0 38.55 0.8945 38.37 0.8874 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

15a,b,c 73.8 72.8 73.0 72.7 73.8 86.4 74.0 0 0 39.82 0.9237 39.76 0.9189 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

16a,b,c 74.0 72.6 72.9 72.6 73.7 87.2 74.0 0 0 40.98 0.9505 40.99 0.9462 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

17a,b,c 74.1 72.4 72.7 72.5 73.5 87.8 74.0 0 0 42.17 0.9779 42.33 0.9775 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

18a,b,c 73.2 72.4 72.6 72.4 73.4 88.7 74.0 0 0 43.46 1.0074 43.66 1.0084 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

19a,b,c 73.6 72.5 72.8 72.4 73.5 89.6 74.0 0 0 44.86 1.0392 44.80 1.0340 orange 9.610 9.210 9.380 9.430 6.690 7.750 0.500 30.00

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.6 74.2 74.3 74.1 74.5 77.9 72.1 0 0 24.06 0.5593 24.07 0.5575 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

2a,b,c 75.9 74.0 74.2 74.0 74.5 78.4 72.1 0 0 25.30 0.5829 25.33 0.5865 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

3a,b,c 75.5 73.7 73.9 73.6 74.3 78.8 72.1 0 0 26.65 0.6193 26.63 0.6167 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

4a,b,c 75.1 73.6 73.7 73.5 74.2 79.1 72.1 0 0 27.93 0.6490 27.94 0.6469 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

5a,b,c 75.0 73.4 73.6 73.3 74.1 79.5 72.1 0 0 29.14 0.6770 29.24 0.6768 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

6a,b,c 74.1 73.1 73.3 73.1 73.9 79.9 72.1 0 0 30.54 0.7095 30.50 0.7060 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

7a,b,c 73.8 72.7 72.9 72.6 73.6 80.3 72.1 0 0 31.86 0.7400 31.78 0.7358 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

8a,b,c 74.3 72.6 72.8 72.5 73.5 80.7 72.1 0 0 33.08 0.7684 33.17 0.7676 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

9a,b,c 74.1 72.5 72.7 72.4 73.3 81.2 72.1 0 0 34.39 0.7985 34.41 0.7964 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

10a,b,c 73.7 72.3 72.6 72.3 73.2 81.6 72.1 0 0 35.72 0.8293 35.72 0.8258 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

11a,b,c 73.4 72.4 72.6 72.4 73.2 82.3 72.1 0 0 37.03 0.8599 37.09 0.8585 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

12a,b,c 73.4 72.5 72.7 72.4 73.2 83.0 72.1 0 0 38.28 0.8885 38.34 0.8868 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

13a,b,c 73.7 72.7 72.9 72.7 73.4 83.9 72.1 0 0 39.65 0.9202 39.59 0.9154 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

14a,b,c 73.9 72.8 73.0 72.8 73.4 84.6 72.1 0 0 41.00 0.9511 40.94 0.9465 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

15a,b,c 74.3 72.9 73.1 72.9 73.4 85.4 72.1 0 0 42.31 0.9813 42.31 0.9777 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

16a,b,c 74.9 72.9 73.1 72.9 73.5 86.2 72.1 0 0 43.61 1.0112 43.56 1.0066 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

17a,b,c 74.3 73.0 73.2 73.0 73.6 87.0 72.1 0 0 44.92 1.0413 44.92 1.0376 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

18a,b,c 75.4 73.2 73.4 73.2 73.7 88.1 72.1 0 0 46.13 1.0691 46.17 1.0660 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

19a,b,c 75.3 73.2 73.4 73.2 73.7 88.9 72.1 0 0 47.37 1.0979 47.46 1.0954 orange 14.090 13.490 13.690 13.790 9.850 11.320 0.750 30.02

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -10

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.4 68.9 69.2 69.0 72.1 75.0 73.6 0 0 25.93 0.6029 25.95 0.6011 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

2a,b,c 73.6 68.3 68.7 68.4 71.5 74.9 73.6 0 0 27.23 0.6329 27.21 0.6302 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

3a,b,c 74.1 68.8 69.1 68.8 71.3 75.5 73.6 0 0 28.50 0.6624 28.49 0.6598 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

4a,b,c 73.5 69.5 69.8 69.5 71.5 76.1 73.6 0 0 29.60 0.6878 29.62 0.6861 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

5a,b,c 74.3 70.4 70.7 70.3 71.6 77.1 73.6 0 0 31.03 0.7209 31.07 0.7192 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

6a,b,c 73.6 70.8 70.9 70.7 71.7 77.8 73.6 0 0 32.51 0.7554 32.54 0.7533 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

7a,b,c 74.3 71.1 71.3 71.1 71.9 78.6 73.6 0 0 33.99 0.7894 34.16 0.7907 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

8a,b,c 73.5 71.2 71.4 71.1 71.9 79.3 73.6 0 0 35.50 0.8245 35.58 0.8234 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

9a,b,c 74.6 71.5 71.6 71.4 72.1 80.0 73.6 0 0 37.01 0.8594 37.00 0.8562 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

10a,b,c 74.3 71.6 71.8 71.4 72.1 81.0 73.6 0 0 38.41 0.8917 38.45 0.8903 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

11a,b,c 74.7 71.6 71.8 71.6 72.1 81.7 73.6 0 0 40.11 0.9304 40.13 0.9280 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

12a,b,c 74.0 71.9 72.1 71.8 72.3 82.5 73.6 0 0 41.49 0.9626 41.48 0.9590 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

13a,b,c 74.6 72.2 72.4 72.2 72.4 83.5 73.6 0 0 43.07 0.9988 43.08 0.9957 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

14a,b,c 75.2 72.2 72.4 72.1 72.5 84.4 73.6 0 0 44.61 1.0345 44.50 1.0283 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

15a,b,c 75.2 72.4 72.6 72.3 72.6 85.3 73.6 0 0 46.06 1.0680 45.97 1.0617 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

16a,b,c 75.0 72.6 72.8 72.5 72.7 86.1 73.6 0 0 47.02 1.0896 47.02 1.0860 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

17a,b,c 74.9 72.8 72.9 72.7 72.9 86.7 73.6 0 0 48.13 1.1154 48.01 1.1083 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

18a,b,c 75.8 72.9 73.0 72.8 73.0 87.6 73.6 0 0 49.12 1.1378 49.11 1.1329 orange 17.61 16.91 17.11 17.21 12.21 14.3 0.78 30.01

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -11

11crossover holes-8 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---8 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 30 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 73.8 73.4 73.5 74.0 0.406 0.389 0.391 0.400 0.276 0.340 water 29.77 0.026 73.2 0

10 73.6 73.4 73.6 74.0 0.654 0.628 0.629 0.644 0.459 0.552 water 29.77 0.038 73.3 0

15 73.8 73.4 73.5 74.0 0.935 0.895 0.909 0.909 0.660 0.788 water 29.77 0.041 73.2 0

20 73.8 73.4 73.4 74.0 3.100 2.990 3.000 3.050 2.240 2.650 orange 29.77 0.19 73.3 0

25 73.8 73.3 73.5 74.0 4.010 3.820 3.900 3.910 2.910 3.430 orange 29.77 0.21 73.3 0

30 73.1 73.3 73.3 74.0 5.020 4.820 4.890 4.960 3.680 4.290 orange 29.77 0.29 73.1 0

40 74.0 73.2 73.4 74.0 7.590 7.290 7.410 7.410 5.490 6.490 orange 29.77 0.4 73.1 0

50 73.9 68.3 68.5 73.9 10.500 10.090 10.280 10.290 7.690 9.040 orange 29.53 0.58 68.4 0

60 73.9 68.4 68.6 73.9 13.710 13.210 13.390 13.490 10.020 11.830 orange 29.53 0.72 68.4 0

70 73.8 68.1 68.3 73.9 17.550 16.950 17.140 17.190 12.870 15.190 orange 29.53 0.88 68.2 0

80 72.7 67.5 67.8 73.9 21.740 20.920 21.140 21.310 15.990 18.620 orange 29.53 1 67.7 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.8 73.3 73.5 73.6 74.6 78.8 71.7 0 0 17.91 0.4163 17.98 0.4166 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

2a,b,c 70.8 73.3 73.5 73.5 74.6 80.1 71.7 0 0 18.84 0.4377 18.78 0.4348 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

3a,b,c 70.8 73.3 73.5 73.4 74.6 80.9 71.7 0 0 19.60 0.4552 19.60 0.4535 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

4a,b,c 70.8 73.3 73.5 73.4 74.6 81.7 71.7 0 0 20.46 0.4752 20.41 0.4728 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

5a,b,c 70.8 73.3 73.5 73.2 74.6 82.7 71.7 0 0 21.18 0.4919 21.18 0.4899 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

6a,b,c 70.8 73.3 73.5 73.2 74.6 83.2 71.7 0 0 22.01 0.5111 22.02 0.5095 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

7a,b,c 70.8 73.3 73.5 73.2 74.6 84.0 71.7 0 0 22.83 0.5302 22.79 0.5272 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

8a,b,c 70.8 73.3 73.5 73.2 74.6 85.0 71.7 0 0 23.65 0.5492 23.61 0.5461 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

9a,b,c 70.8 73.3 73.5 73.2 74.6 85.6 71.7 0 0 24.44 0.5675 24.41 0.5647 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

10a,b,c 70.8 73.3 73.5 73.2 74.6 86.8 71.7 0 0 25.23 0.5860 25.23 0.5833 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

11a,b,c 70.8 73.3 73.5 72.9 74.0 87.5 71.7 0 0 26.04 0.6045 25.99 0.6013 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

12a,b,c 70.8 73.3 73.5 72.9 74.0 88.6 71.7 0 0 26.81 0.6228 26.86 0.6213 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

13a,b,c 70.2 72.0 72.5 72.9 74.0 89.6 71.7 0 0 27.54 0.6393 27.62 0.6385 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

14a,b,c 70.2 72.0 72.5 72.9 74.0 90.3 71.7 0 0 28.47 0.6608 28.41 0.6569 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

15a,b,c 70.2 72.0 72.5 72.9 74.0 91.0 71.7 0 0 29.28 0.6795 29.15 0.6738 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

16a,b,c 70.2 72.0 72.5 72.2 74.0 92.2 71.7 0 0 30.07 0.6977 30.16 0.6967 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

17a,b,c 70.2 72.0 72.5 72.2 74.0 93.8 71.7 0 0 30.95 0.7181 30.99 0.7167 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

18a,b,c 70.2 72.0 72.5 72.2 74.0 94.6 71.7 0 0 31.83 0.7383 31.79 0.7342 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

19a,b,c 70.2 72.0 72.5 72.2 74.0 95.7 71.7 0 0 32.90 0.7630 32.91 0.7599 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

20a,b,c 70.2 72.0 72.5 72.2 74.0 97.4 71.7 0 0 33.73 0.7822 33.78 0.7798 water 0.815 0.779 0.789 0.788 0.57 0.68 0.051 30.06

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -12

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.1 71.6 71.8 71.5 73.0 77.6 74.0 0 0 19.97 0.4638 20.03 0.4638 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

2a,b,c 70.1 71.6 71.8 71.5 73.0 78.4 74.0 0 0 21.01 0.4881 20.94 0.4851 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

3a,b,c 70.1 71.6 71.8 71.5 73.0 79.0 74.0 0 0 21.77 0.5056 21.80 0.5045 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

4a,b,c 70.1 71.6 71.8 71.5 73.0 79.6 74.0 0 0 22.75 0.5285 22.80 0.5277 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

5a,b,c 70.1 71.6 71.8 71.5 73.0 80.2 74.0 0 0 23.59 0.5478 23.60 0.5462 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

6a,b,c 70.1 71.6 71.8 71.5 73.0 80.9 74.0 0 0 24.55 0.5704 24.57 0.5685 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

7a,b,c 70.1 71.6 71.8 71.5 73.0 81.6 74.0 0 0 25.42 0.5902 25.33 0.5867 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

8a,b,c 70.1 71.6 71.8 71.5 73.0 82.1 74.0 0 0 26.17 0.6079 26.17 0.6058 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

9a,b,c 70.1 71.2 71.3 71.5 73.0 82.5 74.0 0 0 27.07 0.6286 27.12 0.6273 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

10a,b,c 70.1 71.2 71.3 71.5 72.6 83.2 74.0 0 0 28.05 0.6512 28.02 0.6485 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

11a,b,c 70.1 71.2 71.3 71.2 72.6 83.9 74.0 0 0 29.12 0.6761 29.05 0.6717 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

12a,b,c 70.1 71.2 71.3 71.2 72.6 84.7 74.0 0 0 30.21 0.7014 30.06 0.6950 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

13a,b,c 70.1 71.2 71.3 71.2 72.6 85.6 74.0 0 0 31.12 0.7222 31.12 0.7196 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

14a,b,c 70.1 71.2 71.3 71.2 72.6 86.3 74.0 0 0 32.34 0.7506 32.30 0.7473 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

15a,b,c 70.1 71.2 71.3 71.2 72.6 87.5 74.0 0 0 33.44 0.7760 33.50 0.7743 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

16a,b,c 70.1 71.2 71.3 71.2 72.6 88.4 74.0 0 0 34.80 0.8074 34.79 0.8040 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

17a,b,c 70.1 71.2 71.3 71.2 72.6 89.7 74.0 0 0 35.94 0.8342 35.83 0.8275 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

18a,b,c 70.1 71.2 71.3 71.2 72.6 91.0 74.0 0 0 37.06 0.8595 37.03 0.8547 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

19a,b,c 70.1 71.2 71.3 71.2 72.6 92.1 74.0 0 0 38.25 0.8870 38.21 0.8823 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

20a,b,c 70.1 71.2 71.3 71.2 72.6 93.6 74.0 0 0 39.43 0.9143 39.32 0.9078 orange 4.3 4.15 4.21 4.2 3.11 3.69 0.24 29.77

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.9 73.2 73.5 73.1 73.9 77.4 74.1 0 0 21.49 0.4992 21.45 0.4967 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

2a,b,c 73.9 73.2 73.5 73.1 73.9 78.1 74.1 0 0 22.52 0.5230 22.51 0.5212 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

3a,b,c 73.9 73.2 73.5 73.1 73.9 78.8 74.1 0 0 23.44 0.5446 23.46 0.5433 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

4a,b,c 73.9 73.2 73.5 73.1 73.9 79.5 74.1 0 0 24.48 0.5687 24.65 0.5705 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

5a,b,c 73.9 73.2 73.5 73.1 73.9 80.1 74.1 0 0 25.58 0.5942 25.45 0.5892 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

6a,b,c 73.9 73.2 73.5 73.1 73.9 80.6 74.1 0 0 26.52 0.6156 26.58 0.6151 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

7a,b,c 73.9 73.2 73.5 73.1 73.9 81.3 74.1 0 0 27.44 0.6373 27.57 0.6381 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

8a,b,c 73.9 73.2 73.5 73.1 73.9 82.0 74.1 0 0 28.44 0.6605 28.50 0.6594 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

9a,b,c 73.9 73.2 73.5 73.1 73.9 82.6 74.1 0 0 29.49 0.6848 29.49 0.6823 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

10a,b,c 73.9 73.2 73.5 73.1 73.9 83.2 74.1 0 0 30.42 0.7066 30.47 0.7047 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

11a,b,c 73.3 73.2 73.5 73.1 73.9 84.0 74.1 0 0 31.50 0.7315 31.50 0.7286 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

12a,b,c 73.3 72.6 73.5 73.1 73.9 84.6 74.1 0 0 32.65 0.7579 32.56 0.7531 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

13a,b,c 73.3 72.6 73.5 71.9 73.9 85.0 74.1 0 0 33.42 0.7758 33.39 0.7726 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

14a,b,c 71.8 72.6 72.1 71.9 73.9 85.7 74.1 0 0 34.43 0.7991 34.49 0.7975 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

15a,b,c 71.8 72.0 72.1 71.9 73.1 86.4 74.1 0 0 35.54 0.8247 35.47 0.8201 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

16a,b,c 71.8 72.0 72.1 71.9 73.1 86.8 74.1 0 0 36.58 0.8488 36.61 0.8463 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

17a,b,c 71.8 72.0 72.1 71.9 73.1 87.6 74.1 0 0 37.50 0.8697 37.40 0.8643 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

18a,b,c 71.8 72.0 72.1 71.9 73.1 88.3 74.1 0 0 38.53 0.8937 38.53 0.8900 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

19a,b,c 71.8 72.0 72.1 71.9 73.1 89.0 74.1 0 0 39.64 0.9194 39.62 0.9152 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

20a,b,c 71.8 72.0 72.1 71.9 73.1 90.4 74.1 0 0 41.00 0.9499 41.02 0.9470 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

21a,b,c 71.3 72 72.1 71.9 73.1 91.5 74.1 42.46 0.9841 42.35 0.9774 orange 7.59 7.29 7.41 7.41 5.49 6.49 0.4 29.98

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -13

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/28/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.3 73.1 73.2 73.0 73.8 77.1 73.1 0 0 23.03 0.5453 23.04 0.5338 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

2a,b,c 74.2 72.9 73.1 72.9 73.8 77.9 73.1 0 0 24.16 0.5613 24.13 0.5582 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

3a,b,c 73.0 72.7 72.9 72.6 73.6 78.2 73.1 0 0 25.23 0.5861 25.20 0.5839 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

4a,b,c 73.3 72.6 72.8 72.6 73.5 78.8 73.1 0 0 26.45 0.6146 26.45 0.6124 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

5a,b,c 73.1 72.5 72.8 72.5 73.5 79.3 73.1 0 0 27.56 0.6400 27.60 0.6390 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

6a,b,c 73.8 72.6 72.8 72.5 73.5 79.9 73.1 0 0 28.83 0.6696 28.83 0.6673 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

7a,b,c 73.3 72.5 72.8 72.5 73.4 80.5 73.1 0 0 29.96 0.6956 29.90 0.6922 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

8a,b,c 72.7 72.4 72.6 72.3 73.3 81.0 73.1 0 0 31.22 0.7248 31.17 0.7211 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

9a,b,c 73.6 72.3 72.5 72.3 73.1 81.5 73.1 0 0 32.20 0.7474 32.25 0.7460 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

10a,b,c 73.9 72.3 72.5 72.2 73.2 82.2 73.1 0 0 33.31 0.7734 33.31 0.7705 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

11a,b,c 72.5 72.1 72.3 72.1 73.0 82.8 73.1 0 0 34.45 0.7995 34.52 0.7985 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

12a,b,c 73.0 72.0 72.2 72.0 72.9 83.3 73.1 0 0 35.64 0.8269 35.62 0.8236 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

13a,b,c 73.0 72.1 72.3 72.1 73.0 84.1 73.1 0 0 36.83 0.8547 36.80 0.8506 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

14a,b,c 73.4 72.1 72.4 72.1 73.0 84.9 73.1 0 0 37.83 0.8778 37.83 0.8743 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

15a,b,c 73.6 72.3 72.5 72.3 73.0 85.7 73.1 0 0 38.96 0.9035 38.90 0.8995 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

16a,b,c 73.4 72.4 72.6 72.4 73.1 86.4 73.1 0 0 40.11 0.9304 40.02 0.9256 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

17a,b,c 74.0 72.5 72.6 72.5 73.1 87.4 73.1 0 0 41.23 0.9556 41.39 0.9559 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

18a,b,c 74.3 72.6 72.7 72.5 73.2 88.3 73.1 0 0 42.43 0.9831 42.53 0.9823 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

19a,b,c 74.5 72.7 72.9 72.6 73.3 89.4 73.1 0 0 43.72 1.0137 43.69 1.0100 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

20a,b,c 73.5 72.9 73.0 72.8 73.4 90.3 73.1 0 0 44.93 1.0405 44.85 1.0357 orange 11.65 11.21 11.35 11.44 8.52 10.04 0.63 29.7

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/27/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.5 73.0 73.2 72.9 73.9 77.0 74.1 0 0 24.02 0.5581 24.08 0.5580 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

2a,b,c 74.1 72.9 73.1 72.9 73.9 77.6 74.1 0 0 25.25 0.5865 25.26 0.5851 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

3a,b,c 74.1 72.7 72.9 72.6 73.7 78.1 74.1 0 0 26.40 0.6133 26.46 0.6126 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

4a,b,c 74.1 72.6 72.8 72.5 73.6 78.4 74.1 0 0 27.69 0.6432 27.69 0.6411 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

5a,b,c 73.8 72.4 72.6 72.3 73.4 78.8 74.1 0 0 28.83 0.6697 28.89 0.6690 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

6a,b,c 74.1 72.5 72.6 72.4 73.5 79.3 74.1 0 0 29.98 0.6961 30.02 0.6949 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

7a,b,c 73.3 72.4 72.6 72.4 73.4 79.8 74.1 0 0 31.21 0.7254 31.26 0.7236 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

8a,b,c 73.4 72.3 72.5 72.3 73.3 80.3 74.1 0 0 32.40 0.7523 32.40 0.7500 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

9a,b,c 73.7 72.3 72.5 72.3 73.3 80.7 74.1 0 0 33.79 0.7842 33.63 0.7781 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

10a,b,c 74.3 72.3 72.5 72.3 73.2 81.4 74.1 0 0 34.88 0.8097 34.87 0.8069 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

11a,b,c 74.2 72.3 72.5 72.3 73.1 81.9 74.1 0 0 36.01 0.8360 35.98 0.8319 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

12a,b,c 74.1 72.3 72.5 72.3 73.1 82.5 74.1 0 0 37.31 0.8657 37.31 0.8629 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

13a,b,c 73.6 72.2 72.4 72.1 73.0 83.1 74.1 0 0 38.45 0.8920 38.46 0.8885 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

14a,b,c 74.2 72.3 72.5 72.3 73.0 83.9 74.1 0 0 39.60 0.9182 39.60 0.9154 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

15a,b,c 74.6 72.5 72.6 72.4 73.1 84.7 74.1 0 0 40.79 0.9460 40.80 0.9433 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

16a,b,c 74.8 72.5 72.7 72.5 73.1 85.5 74.1 0 0 42.15 0.9773 42.04 0.9715 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

17a,b,c 74.2 72.6 72.8 72.6 73.1 86.3 74.1 0 0 43.40 1.0062 43.55 1.0060 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

18a,b,c 74.8 72.8 73.0 72.8 73.3 87.4 74.1 0 0 44.85 1.0394 44.86 1.0367 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

19a,b,c 74.9 72.9 73.1 72.9 73.3 88.2 74.1 0 0 46.21 1.0703 46.12 1.0635 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

20a,b,c 75.4 73.0 73.2 72.9 73.4 89.0 74.1 0 0 47.46 1.0986 47.36 1.0929 orange 17.08 16.43 16.62 16.78 12.51 14.75 0.88 29.65

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -14

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/27/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.7 67.5 67.8 67.7 70.4 73.6 73.9 0 0 25.65 0.5959 25.62 0.5934 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

2a,b,c 73.8 68.1 68.3 68.2 70.3 74.0 73.9 0 0 26.85 0.6239 26.82 0.6211 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

3a,b,c 73.9 68.4 68.6 68.4 70.3 74.6 73.9 0 0 28.05 0.6515 28.04 0.6495 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

4a,b,c 73.9 68.3 68.5 68.4 70.3 75.1 73.9 0 0 29.51 0.6855 29.54 0.6838 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

5a,b,c 74.0 68.7 68.9 68.7 70.4 75.8 73.9 0 0 30.98 0.7191 31.07 0.7194 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

6a,b,c 73.6 69.4 69.6 69.3 70.6 76.7 73.9 0 0 32.49 0.8544 32.58 0.7541 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

7a,b,c 73.6 70.1 70.2 70.0 70.9 77.7 73.9 0 0 33.95 0.7884 33.94 0.7856 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

8a,b,c 73.9 70.6 70.7 70.4 71.2 78.8 73.9 0 0 35.46 0.8231 35.47 0.8210 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

9a,b,c 73.8 71.1 71.2 70.9 71.4 79.7 73.9 0 0 37.06 0.8603 37.03 0.8569 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

10a,b,c 74.9 71.3 71.4 71.1 71.6 80.6 73.9 0 0 38.55 0.8943 38.51 0.8908 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

11a,b,c 74.4 71.6 71.7 71.5 71.8 81.6 73.9 0 0 40.00 0.9278 40.01 0.9253 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

12a,b,c 75.2 71.9 72.0 71.7 72.0 82.8 73.9 0 0 41.56 0.9639 41.54 0.9606 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

13a,b,c 75.4 72.1 72.2 72.0 72.2 83.7 73.9 0 0 43.01 0.9973 43.08 0.9962 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

14a,b,c 75.4 72.3 72.4 72.2 72.4 84.9 73.9 0 0 44.41 1.0293 44.39 1.0255 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

15a,b,c 75.1 72.5 72.5 72.4 72.5 85.6 73.9 0 0 45.39 1.0518 45.52 1.0514 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

16a,b,c 75.9 72.7 72.8 72.6 72.7 86.5 73.9 0 0 46.46 1.0765 46.43 1.0723 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

17a,b,c 75.4 72.8 73.0 72.6 72.8 87.2 73.9 0 0 47.43 1.0982 47.41 1.0945 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

18a,b,c 75.5 72.9 73.0 72.8 72.9 87.7 73.9 0 0 48.37 1.1204 48.41 1.1176 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

19a,b,c 75.6 73.1 73.2 72.8 73.1 88.6 73.9 0 0 49.52 1.1470 49.41 1.1402 orange 21.740 20.920 21.140 21.310 15.990 18.620 1.000 29.53

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -15

11crossover holes-7 exit holes, inline arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---7 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 30 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 73.6 72.8 72.9 74.5 0.215 0.197 0.202 0.209 0.106 0.101 water 30.07 0.024 73.2 0

10 73.5 73.0 73.1 74.5 0.347 0.321 0.320 0.331 0.182 0.169 water 30.07 0.017 72.9 0

15 73.6 73.0 73.1 74.5 0.503 0.468 0.478 0.484 0.279 0.251 water 30.07 0.017 73.0 0

20 73.6 72.8 72.9 74.5 0.681 0.635 0.655 0.663 0.386 0.353 water 30.07 0.021 72.8 0

25 69.5 70.2 70.4 73.8 0.897 0.839 0.860 0.867 0.491 0.468 water 30.23 0.020 70.2 0

30 69.6 70.2 70.4 73.8 2.710 2.530 2.600 2.650 1.500 1.410 orange 30.23 0.050 70.1 0

40 69.8 69.8 70.0 73.8 4.020 3.770 3.860 3.890 2.320 2.120 orange 30.23 0.100 69.7 0

50 69.8 69.9 70.1 73.8 5.560 5.190 5.320 5.390 3.250 2.930 orange 30.23 0.170 70.0 0

60 69.5 70.1 70.3 73.8 7.150 6.820 7.020 7.110 4.290 3.890 orange 30.23 0.210 69.8 0

70 73.5 72.2 72.4 74.6 9.290 8.700 8.930 8.990 5.450 4.990 orange 30.21 0.200 72.1 0

80 76.9 74.5 74.7 73.6 11.550 10.740 10.990 11.180 6.780 6.190 orange 30.22 0.210 74.4 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/26/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.6 73.4 73.6 73.4 74.2 79.2 71.0 0 0 17.51 0.4064 17.56 0.4063 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

2a,b,c 73.6 73.4 73.6 73.4 74.2 80.0 71.0 0 0 18.10 0.4204 18.13 0.4197 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

3a,b,c 73.6 73.4 73.6 73.4 74.2 80.6 71.0 0 0 18.70 0.4344 18.73 0.4333 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

4a,b,c 73.6 73.4 73.6 73.4 74.2 81.5 71.0 0 0 19.35 0.4493 19.26 0.4457 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

5a,b,c 73.6 73.4 73.6 73.4 74.2 82.2 71.0 0 0 19.97 0.4697 19.89 0.4602 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

6a,b,c 73.6 73.4 73.6 73.4 74.2 82.7 71.0 0 0 20.63 0.4788 20.46 0.4732 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

7a,b,c 72.5 73.4 73.6 73.4 74.2 83.3 71.0 0 0 21.13 0.4909 21.16 0.4891 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

8a,b,c 72.5 73.4 73.6 73.4 74.2 83.9 71.0 0 0 21.71 0.5041 21.69 0.5017 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

9a,b,c 72.5 73.4 73.6 73.4 74.2 84.5 71.0 0 0 22.42 0.5207 22.43 0.5185 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

10a,b,c 72.5 73.4 73.6 73.4 74.2 85.2 71.0 0 0 22.97 0.5333 22.95 0.5308 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

11a,b,c 72.5 73.4 73.6 73.4 74.2 86.0 71.0 0 0 23.46 0.5450 23.54 0.5444 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

12a,b,c 72.5 73.4 73.6 73.4 74.2 86.6 71.0 0 0 24.10 0.5597 24.08 0.5568 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

13a,b,c 72.5 73.4 73.6 73.4 74.2 87.4 71.0 0 0 24.78 0.5752 24.76 0.5727 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

14a,b,c 72.5 73.4 73.6 73.4 74.2 88.0 71.0 0 0 25.37 0.5888 25.35 0.5866 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

15a,b,c 72.5 73.4 73.6 73.4 74.2 88.6 71.0 0 0 25.97 0.6030 26.00 0.6011 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

16a,b,c 72.5 73.4 73.6 73.4 74.2 89.5 71.0 0 0 26.56 0.6165 26.54 0.6137 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

17a,b,c 72.5 73.4 73.6 73.4 74.2 90.3 71.0 0 0 27.16 0.6303 27.12 0.6266 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

18a,b,c 72.5 73.4 73.6 73.4 74.2 91.0 71.0 0 0 27.70 0.6429 27.80 0.6425 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

19a,b,c 72.5 73.4 73.6 73.4 74.2 91.9 71.0 0 0 28.39 0.6591 28.42 0.6568 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

20a,b,c 72.5 73.4 73.6 73.4 74.2 92.7 71.0 0 0 28.95 0.6717 28.96 0.6693 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

21a,b,c 72.5 73.4 73.6 73.4 74.2 93.6 71.0 0 0 29.50 0.6844 29.57 0.6832 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

22a,b,c 72.5 73.4 73.6 73.4 74.2 94.6 71.0 0 0 30.17 0.6998 30.13 0.6960 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

23a,b,c 72.5 73.4 73.6 73.4 74.2 95.1 71.0 0 0 30.70 0.7123 30.71 0.7093 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

24a,b,c 72.5 73.4 73.6 73.4 74.2 96.5 71.0 0 0 31.49 0.7305 31.43 0.7259 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

25a,b,c 72.4 73.4 73.6 73.4 74.2 97.3 71.0 0 0 32.20 0.7469 32.07 0.7406 orange 2.5 2.43 2.46 2.49 1.91 2.26 0.14 29.66

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -16

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/26/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.3 73.5 73.6 73.4 73.8 77.4 70.0 0 0 19.98 0.4642 20.04 0.4639 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

2a,b,c 76.2 73.6 73.7 73.5 73.9 78.7 70.0 0 0 20.81 0.4833 20.89 0.4836 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

3a,b,c 76.2 73.6 73.9 73.7 73.7 79.6 70.0 0 0 21.62 0.5024 21.63 0.5006 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

4a,b,c 77.0 74.9 74.9 74.4 73.9 81.5 70.0 0 0 22.51 0.5227 22.45 0.5196 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

5a,b,c 77.0 74.9 74.9 74.4 73.9 82.2 70.0 0 0 23.26 0.5402 23.29 0.5389 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

6a,b,c 77.0 74.9 74.9 74.4 74.6 82.7 70.0 0 0 24.06 0.5587 24.05 0.5565 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

7a,b,c 77.0 74.9 74.9 74.4 74.6 83.3 70.0 0 0 24.89 0.5779 24.85 0.5753 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

8a,b,c 77.0 74.9 74.9 74.4 74.6 84.1 70.0 0 0 25.62 0.5954 25.60 0.5922 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

9a,b,c 77.0 74.9 74.9 74.4 74.6 84.8 70.0 0 0 26.39 0.6132 26.48 0.6126 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

10a,b,c 77.0 74.9 74.9 74.4 74.6 85.3 70.0 0 0 27.19 0.6313 27.22 0.6296 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

11a,b,c 77.0 75.5 75.2 75.3 75.6 86.2 70.0 0 0 28.13 0.6530 28.03 0.6483 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

12a,b,c 77.0 75.5 75.2 75.3 75.6 87.2 70.0 0 0 28.78 0.6679 28.72 0.6641 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

13a,b,c 77.0 75.5 75.2 75.3 75.6 88.3 70.0 0 0 29.62 0.6875 29.68 0.6862 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

14a,b,c 77.0 75.5 75.2 75.3 75.6 89.1 70.0 0 0 30.47 0.7071 30.47 0.7045 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

15a,b,c 77.0 75.5 75.2 75.3 75.6 89.9 70.0 0 0 31.27 0.7255 31.23 0.7210 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

16a,b,c 77.0 75.5 75.2 75.3 75.6 91.0 70.0 0 0 32.12 0.7448 32.04 0.7403 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

17a,b,c 77.0 75.5 75.2 75.3 75.6 92.2 70.0 0 0 32.78 0.7600 32.90 0.7598 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

18a,b,c 77.0 75.5 75.2 75.3 75.6 92.8 70.0 0 0 33.59 0.7793 33.63 0.7770 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

19a,b,c 77.0 75.5 75.2 75.3 75.6 93.6 70.0 0 0 34.46 0.7994 34.42 0.7950 orange 5.29 5.09 5.12 5.19 4.05 4.83 0.19 29.92

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/20/2012

40 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.9 73.2 73.3 73 73.5 77.3 74 0 0 20.51 0.4765 20.53 0.4755 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

2a,b,c 75.8 73.2 73.3 73.1 73.5 77.8 74 0 0 21.5 0.4996 21.55 0.4986 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

3a,b,c 75.8 73.2 73.3 73.3 73.5 78.4 74 0 0 22.29 0.5177 22.29 0.5159 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

4a,b,c 75.8 73.2 73.3 73.5 73.6 78.9 74 0 0 23.05 0.5355 23.04 0.5332 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

5a,b,c 75.8 74.2 74.6 74.4 73.7 79.7 74 0 0 23.76 0.552 23.77 0.5501 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

6a,b,c 75.8 74.2 74.6 74.4 74 80.4 74 0 0 24.6 0.5713 24.68 0.5712 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

7a,b,c 75.8 74.2 74.6 74.4 74.1 81.1 74 0 0 25.41 0.5902 25.38 0.5876 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

8a,b,c 75.8 74.2 74.6 74.4 74.7 81.6 74 0 0 26.17 0.6077 26.23 0.6071 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

9a,b,c 75.8 74.2 74.6 74.4 74.7 82.3 74 0 0 27.03 0.6277 27.1 0.627 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

10a,b,c 75.8 74.2 74.6 74.4 74.7 83 74 0 0 27.79 0.6453 27.85 0.6446 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

11a,b,c 75.8 74.2 74.6 74.4 74.7 83.7 74 0 0 28.66 0.6654 28.63 0.6622 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

12a,b,c 75.8 74.2 74.6 74.4 74.7 84.2 74 0 0 29.43 0.6832 29.52 0.6826 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

13a,b,c 75.8 74.2 74.6 74.4 74.7 84.8 74 0 0 30.41 0.7049 30.43 0.7036 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

14a,b,c 75.8 74.2 74.6 74.4 74.7 85.5 74 0 0 31.39 0.7287 31.32 0.7243 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

15a,b,c 75.8 74.2 74.6 74.4 74.7 86.1 74 0 0 32.22 0.7479 32.23 0.7452 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

16a,b,c 75.8 74.2 74.6 74.4 74.7 86.8 74 0 0 33.21 0.7706 33.19 0.7673 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

17a,b,c 75.8 74.2 74.6 74.4 74.7 87.8 74 0 0 34.1 0.7912 34.15 0.7897 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

18a,b,c 75.8 74.2 74.6 74.4 74.7 88.4 74 0 0 358.2 0.8167 35.17 0.8128 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

19a,b,c 75.8 74.2 74.6 74.4 74.7 89.2 74 0 0 36.27 0.8414 36.22 0.8373 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

20a,b,c 75.8 74.2 74.6 74.4 74.7 90.3 74 0 0 37.2 0.863 37.31 0.8619 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

21a,b,c 75.8 74.2 74.6 74.4 74.7 90.9 74 0 0 38.18 0.8853 38.2 0.8822 orange 9.41 9.11 9.26 9.29 7.21 8.49 0.33 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -17

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/19/2012

54 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 79.4 76.3 76.4 76.2 76.2 79.2 73.4 0 0 20.64 0.4795 20.62 0.4775 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

2a,b,c 80.2 76.7 76.8 76.5 76.4 80.2 73.4 0 0 21.67 0.5034 21.65 0.5011 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

3a,b,c 79.7 76.8 76.9 76.7 76.5 80.8 73.4 0 0 22.6 0.5249 22.57 0.5227 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

4a,b,c 80.4 76.9 77 76.8 76.6 81.3 73.4 0 0 23.63 0.5488 23.63 0.5467 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

5a,b,c 79.8 77.2 77.3 77.1 76.8 81.9 73.4 0 0 24.44 0.5678 24.54 0.568 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

6a,b,c 79.4 77.2 77.2 77 76.8 82.4 73.4 0 0 25.61 0.5948 25.61 0.5929 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

7a,b,c 79.3 77.1 77.2 77 76.8 82.9 73.4 0 0 26.43 0.6139 26.48 0.6129 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

8a,b,c 79.5 77 77.2 76.9 76.8 83.3 73.4 0 0 27.57 0.6401 27.56 0.6378 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

9a,b,c 78.9 76.9 77.1 76.8 76.8 83.8 73.4 0 0 28.51 0.662 28.58 0.6613 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

10a,b,c 79.4 76.9 77 76.8 76.7 84.4 73.4 0 0 29.56 0.6862 29.49 0.682 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

11a,b,c 79.1 76.6 76.7 76.5 76.6 85 73.4 0 0 30.43 0.7065 30.49 0.7052 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

12a,b,c 78.3 76.5 76.6 76.4 76.5 85.4 73.4 0 0 31.43 0.7296 31.47 0.7279 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

13a,b,c 78.5 76.5 76.6 76.4 76.5 86.1 73.4 0 0 32.48 0.754 32.47 0.7508 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

14a,b,c 78.3 76.4 76.6 76.4 76.5 86.5 73.4 0 0 33.57 0.779 33.63 0.7775 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

15a,b,c 78.4 76.2 76.4 76.2 76.3 86.9 73.4 0 0 34.51 0.8008 34.46 0.7969 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

16a,b,c 78.2 76.2 76.3 76.2 76.3 87.7 73.4 0 0 35.56 0.8251 35.51 0.8212 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

17a,b,c 78.6 76.1 76.2 76 76.2 88.2 73.4 0 0 36.48 0.8463 36.58 0.8453 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

18a,b,c 78.1 76.1 76.2 76.1 76.2 89 73.4 0 0 37.56 0.8712 37.65 0.8702 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

19a,b,c 78 76 76.1 76 76.1 89.5 73.4 0 0 38.46 0.8921 38.5 0.8895 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

20a,b,c 78.1 76 76.1 75.9 76.1 90.2 73.4 0 0 39.62 0.9189 39.53 0.9133 orange 14.57 14.17 14.33 14.39 11.27 13.19 0.45 30.03

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/19/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 78.6 75.1 75.2 74.9 75.3 78.3 70.9 0 0 21.63 0.5025 21.7 0.5026 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

2a,b,c 78.1 75.3 75.4 75.1 75.3 78.9 70.9 0 0 22.71 0.5276 22.78 0.5274 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

3a,b,c 78.2 75.4 75.5 75.2 75.4 79.4 70.9 0 0 23.81 0.5532 23.78 0.5505 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

4a,b,c 77.9 75.4 75.6 75.3 75.4 79.8 70.9 0 0 24.87 0.5779 24.74 0.5727 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

5a,b,c 77.5 75.3 75.5 75.3 75.3 80.2 70.9 0 0 25.78 0.5987 25.86 0.5985 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

6a,b,c 77.4 75.3 75.4 75.2 75.3 80.6 70.9 0 0 26.87 0.6242 26.88 0.6223 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

7a,b,c 77.9 75.2 75.4 75.2 75.3 81 70.9 0 0 27.81 0.6458 27.85 0.645 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

8a,b,c 77.4 75.1 75.2 75 75.2 81.4 70.9 0 0 28.9 0.6711 28.85 0.6683 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

9a,b,c 77.4 75.2 75.3 75.1 75.2 81.9 70.9 0 0 29.92 0.6946 29.92 0.693 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

10a,b,c 78 75.1 75.2 75 75.2 82.4 70.9 0 0 30.87 0.7169 30.87 0.7143 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

11a,b,c 78 75.1 75.3 75.1 75.2 82.9 70.9 0 0 31.84 0.7393 31.81 0.7362 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

12a,b,c 78.3 75.2 75.4 75.2 75.2 83.4 70.9 0 0 32.98 0.7655 32.98 0.763 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

13a,b,c 78.8 75.6 75.7 75.5 75.5 84.2 70.9 0 0 33.96 0.7881 34.03 0.7872 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

14a,b,c 78.3 75.7 75.8 75.6 75.5 85.1 70.9 0 0 35.13 0.8152 35.17 0.8133 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

15a,b,c 79 75.8 75.9 75.7 75.6 85.5 70.9 0 0 36.21 0.8403 36.27 0.8384 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

16a,b,c 79.1 75.9 76 75.8 75.7 86.3 70.9 0 0 37.3 0.8653 37.34 0.8629 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

17a,b,c 78.8 76 76.1 75.9 75.8 86.9 70.9 0 0 38.31 0.8884 38.23 0.8837 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

18a,b,c 79.2 76.1 76.2 76 75.9 88 70.9 0 0 39.34 0.9124 39.23 0.9057 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

19a,b,c 79.1 76.3 76.4 76.2 76 88.5 70.9 0 0 40.47 0.9387 40.41 0.9339 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

20a,b,c 79 76.4 76.5 76.3 76.2 89.3 70.9 0 0 41.49 0.9619 41.57 0.9602 orange 21.15 20.55 20.81 20.83 16.31 19.19 0.8 30.05

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -18

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/19/2012

80 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.6 73.9 74.1 73.8 74 77 74.2 0 0 22.24 0.5167 22.14 0.5125 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

2a,b,c 76.1 74.2 74.2 74 74.1 77.5 74.2 0 0 23.07 0.5359 23.08 0.5344 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

3a,b,c 76.9 74.2 74.2 74.1 74.2 78 74.2 0 0 24.11 0.56 24.14 0.5591 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

4a,b,c 76.3 74.2 74.3 74 74.3 78.5 74.2 0 0 25.31 0.5878 25.39 0.5877 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

5a,b,c 77 74.4 74.5 74.2 74.4 79 74.2 0 0 26.47 0.6149 26.48 0.6133 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

6a,b,c 77.4 74.5 74.6 74.3 74.5 79.6 74.2 0 0 27.69 0.6433 27.6 0.649 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

7a,b,c 76.5 74.6 74.7 74.3 74.6 80.2 74.2 0 0 28.73 0.6673 28.8 0.6667 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

8a,b,c 76.7 74.6 74.7 74.5 74.7 80.8 74.2 0 0 29.97 0.6959 30 0.6943 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

9a,b,c 77.4 74.6 74.8 74.5 74.7 81.3 74.2 0 0 31.2 0.7426 31.2 0.7221 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

10a,b,c 77.3 74.7 74.8 74.6 74.7 81.8 74.2 0 0 32.41 0.7523 32.33 0.7483 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

11a,b,c 78.3 75.1 75.3 75 75 83.1 74.2 0 0 33.59 0.7798 33.53 0.776 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

12a,b,c 78.2 75.4 75.5 75.3 75.1 83.7 74.2 0 0 34.62 0.8034 34.62 0.8006 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

13a,b,c 78.2 75.5 75.6 75.4 75.2 84.2 74.2 0 0 35.76 0.8299 35.72 0.826 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

14a,b,c 78.8 75.7 75.8 75.6 75.4 84.8 74.2 0 0 36.78 0.8537 36.83 0.8528 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

15a,b,c 79.2 75.8 75.9 75.7 75.4 85.6 74.2 0 0 37.95 0.8804 37.96 0.8776 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

16a,b,c 79.3 76 76.1 75.9 75.7 86.3 74.2 0 0 39.11 0.9073 39.14 0.905 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

17a,b,c 79.5 76.1 76.1 75.9 75.7 87.2 74.2 0 0 40.16 0.9315 40.23 0.9298 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

18a,b,c 78.8 76.1 76.2 75.9 75.8 87.9 74.2 0 0 41.51 0.9626 41.56 0.96 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

19a,b,c 78.8 76.1 76.2 76 75.9 88.9 74.2 0 0 42.66 0.989 42.73 0.9871 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

20a,b,c 78.9 76.2 76.3 76.1 76 89.4 74.2 0 0 43.97 1.019 43.86 1.0131 orange 26.52 25.79 26.22 26.23 20.49 24.11 0.94 30.1

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -19

11crossover holes-12 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 5 degree 11 cross-over holes---12 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 03 / 26 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 75.4 71.9 72.1 69.2 0.209 0.189 0.197 0.203 0.103 0.105 water 29.74 0 72.1 0

10 75.4 71.9 72.1 69.2 0.342 0.322 0.328 0.336 0.18 0.18 water 29.74 0 72.1 0

15 75.4 71.9 72.1 69.2 0.505 0.458 0.468 0.481 0.256 0.256 water 29.74 0 72.1 0

20 75.4 71.9 72.1 69.2 0.662 0.614 0.631 0.642 0.342 0.342 water 29.74 0 72.1 0

25 75.4 71.9 72.1 69.2 0.836 0.771 0.788 0.796 0.431 0.431 water 29.74 0 72.1 0

30 75.4 71.9 72.1 69.2 2.61 2.43 2.51 2.53 0.561 0.561 water/orange 29.74 0 72.1 0

40 75.4 71.9 72.1 69.2 3.76 3.49 3.59 3.63 1.96 1.96 orange 29.74 0 72.1 0

50 75.4 71.9 72.1 69.2 5.31 4.94 5.11 5.17 2.78 2.78 orange 29.74 0 72.1 0

60 75.4 71.9 72.1 69.2 7.05 6.55 6.71 6.8 3.61 3.61 orange 29.74 0 72.1 0

70 75.4 71.9 72.1 69.2 8.96 8.32 8.6 8.66 4.6 4.6 orange 29.74 0 72.1 0

80 75.4 71.9 72.1 69.2 11.02 10.23 10.54 10.59 5.6 5.6 orange 29.74 0 72.1 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

13 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.6 70.1 70.3 70.1 71 81.9 71.4 0 0 23.51 0.5454 23.45 0.5423 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

2a,b,c 69.9 70.1 70.3 70.1 71 84.9 71.4 0 0 24.08 0.5589 24.06 0.5562 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

3a,b,c 70.2 70.2 70.4 70.2 71.1 86.3 71.4 0 0 24.8 0.5751 24.8 0.5735 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

4a,b,c 70.6 70.4 70.5 70.3 71.2 87.7 71.4 0 0 25.56 0.5927 25.57 0.5909 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

5a,b,c 70.2 70.5 70.6 70.4 71.3 89.3 71.4 0 0 26.23 0.6085 26.21 0.606 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

6a,b,c 70.7 70.5 70.7 70.4 71.4 90.5 71.4 0 0 26.91 0.624 26.92 0.6218 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

7a,b,c 70.5 70.5 70.7 70.4 71.4 91.9 71.4 0 0 27.6 0.6396 27.53 0.6358 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

8a,b,c 70.2 70.6 70.7 70.5 71.4 93.3 71.4 0 0 28.35 0.6573 28.31 0.6531 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

9a,b,c 70.7 70.6 70.7 70.6 71.5 94.9 71.4 0 0 28.91 0.6701 28.95 0.6678 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

10a,b,c 70.1 70.6 70.8 70.5 71.5 96.9 71.4 0 0 29.51 0.6839 29.47 0.6804 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

11a,b,c 70.1 70.6 70.8 70.6 71.5 97.6 71.4 0 0 30.06 0.6966 30.1 0.6944 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

12a,b,c 70.4 70.7 70.8 70.7 71.5 98.9 71.4 0 0 30.94 0.7169 30.79 0.7109 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

13a,b,c 70.7 70.7 70.9 70.8 71.6 100.1 71.4 0 0 31.62 0.7325 31.64 0.7297 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

14a,b,c 70.6 70.6 70.8 70.5 71.6 103.3 71.4 0 0 32.41 0.7507 32.3 0.745 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

15a,b,c 69.8 70.6 70.8 70.6 71.6 104.8 71.4 0 0 33.09 0.7664 33.1 0.763 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

16a,b,c 70.1 70.7 70.9 70.6 71.7 106 71.4 0 0 33.83 0.7838 33.79 0.7787 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

17a,b,c 70 70.6 70.8 70.6 71.6 107.7 71.4 0 0 34.45 0.7968 34.42 0.7929 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

18a,b,c 70.4 70.7 70.9 70.6 71.7 109.1 71.4 0 0 35.22 0.8154 35.22 0.8113 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

19a,b,c 69.8 70.6 70.8 70.6 71.6 110.9 71.4 0 0 35.93 0.8314 35.98 0.829 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

20a,b,c 69.7 70.8 70.9 70.7 71.7 112.1 71.4 0 0 36.6 0.8476 36.55 0.8421 water 0.43 0.391 0.412 0.415 0.228 0.223 0 29.74

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -20

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

26 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.3 70.4 70.5 70.3 71.4 81.7 68.3 0 0 24.46 0.5675 24.32 0.5622 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

2a,b,c 71.1 70.2 70.5 70.2 71.4 83.1 68.3 0 0 25.08 0.582 25.12 0.5809 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

3a,b,c 70.8 70.5 70.6 70.4 71.5 84.5 68.3 0 0 25.91 0.6011 25.8 0.5966 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

4a,b,c 71.2 70.5 70.6 70.4 71.4 85.5 68.3 0 0 26.6 0.6172 26.64 0.6157 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

5a,b,c 70.5 70.3 70.5 70.3 71.4 86.6 68.3 0 0 27.42 0.6359 27.37 0.6326 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

6a,b,c 70.9 70.3 70.5 70.3 71.3 87.6 68.3 0 0 28.2 0.6544 28.1 0.6488 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

7a,b,c 70.3 70.3 70.5 70.2 71.3 89.1 68.3 0 0 28.88 0.6696 28.86 0.6666 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

8a,b,c 70.3 70.3 70.5 70.3 71.3 90.3 68.3 0 0 29.63 0.687 29.62 0.6835 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

9a,b,c 71.1 70.5 70.7 70.4 71.4 91.4 68.3 0 0 30.3 0.7026 30.42 0.7025 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

10a,b,c 70.4 70.4 70.6 70.4 71.3 92.5 68.3 0 0 31.25 0.7245 31.2 0.7203 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

11a,b,c 70.1 70.4 70.6 70.3 71.3 94 68.3 0 0 32.03 0.7423 31.89 0.7363 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

12a,b,c 70.2 70.5 70.7 70.5 71.4 95.2 68.3 0 0 32.64 0.7567 32.66 0.7538 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

13a,b,c 70.9 70.5 70.6 70.4 71.4 96.5 68.3 0 0 33.56 0.7775 33.53 0.7732 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

14a,b,c 70.4 70.4 70.5 70.4 71.3 97.8 68.3 0 0 34.24 0.7936 34.33 0.7917 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

15a,b,c 70.9 70.3 70.5 70.3 71.3 98.9 68.3 0 0 35.16 0.8143 35.26 0.8129 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

16a,b,c 70.2 70.3 70.5 70.2 71.3 100.4 68.3 0 0 36.02 0.8344 36.15 0.8332 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

17a,b,c 70.3 70.3 70.5 70.2 71.3 102.2 68.3 0 0 37.03 0.8574 36.95 0.8513 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

18a,b,c 70.9 70.3 70.5 70.2 71.2 103.7 68.3 0 0 37.72 0.8729 37.9 0.8732 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

19a,b,c 70.8 70.3 70.5 70.2 71.2 105.7 68.3 0 0 38.97 0.9019 38.96 0.8978 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

20a,b,c 70.7 70.5 70.7 70.5 71.3 107.3 68.3 0 0 39.97 0.924 40.04 0.9221 orange 2.13 1.97 2.06 2.09 1.11 1.11 0 29.75

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ staggered 11cross-12exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:03/30/2012

40 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.1 70.8 71 70.7 71.5 83.7 70.1 0 0 26.14 0.6066 26.04 0.6021 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

2a,b,c 72.4 70.8 71 70.7 71.4 84.6 70.1 0 0 26.99 0.6261 26.88 0.6214 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

3a,b,c 72.4 70.9 71.1 70.8 71.4 85.5 70.1 0 0 27.76 0.6439 27.75 0.6411 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

4a,b,c 73.1 71 71.2 70.9 71.4 86.5 70.1 0 0 28.55 0.6622 28.52 0.6588 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

5a,b,c 72.3 71 71.2 70.9 71.5 87.4 70.1 0 0 29.38 0.6814 29.42 0.6801 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

6a,b,c 72.9 71.1 71.2 71 71.5 88.2 70.1 0 0 30.18 0.6991 30.23 0.6983 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

7a,b,c 72.1 71.1 71.2 71 71.5 89.3 70.1 0 0 30.95 0.7176 30.96 0.7154 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

8a,b,c 72 71.1 71.2 71 71.5 90.4 70.1 0 0 31.72 0.7354 31.84 0.735 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

9a,b,c 72.2 71 71.2 70.9 71.5 91.6 70.1 0 0 32.76 0.7592 32.7 0.7549 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

10a,b,c 71.3 71 71.1 70.9 71.5 93 70.1 0 0 33.58 0.7779 33.58 0.7753 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

11a,b,c 71.4 70.9 71.1 70.8 71.5 94.5 70.1 0 0 34.25 0.7934 34.36 0.7926 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

12a,b,c 70.8 70.7 70.9 70.6 71.3 95.1 70.1 0 0 35.25 0.8167 35.18 0.8116 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

13a,b,c 70.8 70.6 70.8 70.6 71.3 96.1 70.1 0 0 35.98 0.8334 36.01 0.8302 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

14a,b,c 70.7 70.6 70.9 70.6 71.4 97.8 70.1 0 0 36.85 0.8526 36.92 0.8523 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

15a,b,c 71.2 70.7 70.8 70.7 71.3 99.5 70.1 0 0 38.19 0.884 38.07 0.8776 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

16a,b,c 71.7 70.6 70.8 70.6 71.3 100.8 70.1 0 0 39.02 0.9032 39.06 0.9006 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

17a,b,c 71.1 70.6 70.8 70.6 71.2 101.6 70.1 0 0 40.15 0.9292 40.18 0.9254 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

18a,b,c 71.2 70.4 70.6 70.4 71.2 102.8 70.1 0 0 41.13 0.9512 41.11 0.9464 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

19a,b,c 71.8 70.4 70.6 70.4 71.1 104.7 70.1 0 0 42.3 0.9786 42.2 0.9717 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

20a,b,c 71 70.4 70.6 70.4 71.2 106.9 70.1 0 0 43.36 1.0029 43.5 1.001 orange 3.76 3.49 3.59 3.63 1.96 1.96 0 29.77

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -21

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

54 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73 70.9 71 70.8 71.4 80.9 69.9 0 0 27.78 0.6445 27.69 0.6403 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

2a,b,c 73.7 71.1 71.2 71 71.5 82 69.9 0 0 28.66 0.6653 28.79 0.6657 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

3a,b,c 74.7 71.4 71.6 71.2 71.6 83.9 69.9 0 0 29.75 0.69 29.82 0.6886 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

4a,b,c 73.8 71.6 71.8 71.6 71.8 85.3 69.9 0 0 30.66 0.7109 30.73 0.7101 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

5a,b,c 74.4 71.8 71.9 71.7 71.8 86.1 69.9 0 0 31.66 0.7346 31.75 0.733 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

6a,b,c 74.1 71.6 71.8 71.6 71.8 87.6 69.9 0 0 32.68 0.7576 32.68 0.7549 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

7a,b,c 73.1 71.6 71.8 71.5 71.8 88.5 69.9 0 0 33.65 0.78 33.63 0.7765 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

8a,b,c 72.7 71.6 71.7 71.5 71.8 89.5 69.9 0 0 34.49 0.7993 34.56 0.7978 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

9a,b,c 72.4 71.6 71.7 71.4 71.8 90.9 69.9 0 0 35.63 0.8251 35.62 0.822 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

10a,b,c 72.7 71.5 71.6 71.4 71.7 92 69.9 0 0 36.63 0.8484 36.67 0.846 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

11a,b,c 73 71.4 71.5 71.3 71.7 93.5 69.9 0 0 37.3 0.8641 37.41 0.8627 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

12a,b,c 72.9 71.4 71.5 71.3 71.7 94.1 69.9 0 0 38.25 0.8854 38.16 0.8801 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

13a,b,c 73.1 71.3 71.5 71.3 71.8 95.6 69.9 0 0 38.98 0.9024 39.02 0.8995 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

14a,b,c 72.6 71.3 71.5 71.2 71.6 96.4 69.9 0 0 39.83 0.9216 39.79 0.9172 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

15a,b,c 73 71.3 71.5 71.2 71.7 97.6 69.9 0 0 40.64 0.9407 40.65 0.9369 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

16a,b,c 72.5 71.1 71.3 71.1 71.5 98.4 69.9 0 0 41.32 0.9555 41.44 0.9545 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

17a,b,c 72.5 71.1 71.3 71.1 71.6 99.1 69.9 0 0 42.24 0.9774 42.16 0.9711 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

18a,b,c 72.3 71.1 71.3 71.1 71.6 100.5 69.9 0 0 43.09 0.9968 43.05 0.9916 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

19a,b,c 73 71.1 71.3 71.1 71.5 101.5 69.9 0 0 43.91 1.0154 43.95 1.0119 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

20a,b,c 72.9 71.1 71.3 71.1 71.5 103.4 69.9 0 0 45.18 1.0446 45.3 1.0422 orange 5.89 5.49 5.59 5.69 3.03 3.03 0 29.84

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11 cross 12 exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.1 71.3 71.5 71.2 71.9 80.8 69.5 0 0 28.76 0.6674 28.82 0.6667 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

2a,b,c 74.8 71.7 71.8 71.6 72 82.7 69.5 0 0 29.98 0.6953 30.04 0.6944 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

3a,b,c 75.7 71.7 71.9 71.6 72 83.6 69.5 0 0 31 0.7185 31.03 0.7173 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

4a,b,c 75 72 72.2 71.9 72.1 84.7 69.5 0 0 32.17 0.7459 32.09 0.7411 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

5a,b,c 75.8 72.2 72.4 72.1 72.2 85.7 69.5 0 0 33.13 0.7681 33.05 0.7634 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

6a,b,c 74.9 72.4 72.5 72.3 72.3 87.1 69.5 0 0 34.04 0.7888 34.08 0.7868 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

7a,b,c 74.6 72.5 72.6 72.4 72.3 88.3 69.5 0 0 35.1 0.8134 35.12 0.8112 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

8a,b,c 75.2 72.5 72.6 72.4 72.3 89.6 69.5 0 0 36.08 0.836 36.16 0.8348 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

9a,b,c 74.3 72.4 72.5 72.3 72.3 90.4 69.5 0 0 37.16 0.8068 37.06 0.8555 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

10a,b,c 74.1 72.3 72.5 72.2 72.3 90.9 69.5 0 0 38.32 0.8869 38.2 0.8814 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

11a,b,c 74.3 72.2 72.4 72.2 72.3 92.2 69.5 0 0 39.27 0.9083 39.04 0.9003 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

12a,b,c 73.7 72.1 72.2 72 72.2 93 69.5 0 0 40.22 0.931 40.13 0.9253 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

13a,b,c 74.8 72 72.1 71.9 72.2 94.3 69.5 0 0 41.16 0.9519 41.13 0.9477 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

14a,b,c 74.7 72 72.2 72 72.1 95.5 69.5 0 0 42.01 0.9712 42.1 0.9708 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

15a,b,c 74.1 72.1 72.3 72 72.2 96.5 69.5 0 0 43.19 0.9991 43.14 0.9937 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

16a,b,c 74.1 72.2 72.4 72.2 72.3 98 69.5 0 0 44.04 1.0193 44.17 1.0174 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

17a,b,c 74.5 72.2 72.4 72.2 72.3 99.8 69.5 0 0 45.14 1.0436 45.07 1.0378 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

18a,b,c 73.8 72.1 72.3 72.1 72.2 100.5 69.5 0 0 46.14 1.0668 46.21 1.0643 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

19a,b,c 73.7 72 72.2 72 72.3 101.8 69.5 0 0 47.13 1.0896 47 1.082 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

20a,b,c 74 72 72.1 71.9 72.2 103.4 69.5 0 0 48.09 1.1112 48.26 1.1107 orange 8.59 7.98 8.21 8.21 4.4 4.4 0 29.92

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -22

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

80 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.4 71.9 72.1 71.9 72.2 80.4 69.2 0 0 30.12 0.6986 30.18 0.6976 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

2a,b,c 76.2 72.2 72.3 72.1 72.3 82.4 69.2 0 0 31.09 0.7211 31.05 0.7179 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

3a,b,c 75.7 72.5 72.6 72.4 72.4 83.5 69.2 0 0 32.16 0.7456 32.17 0.7433 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

4a,b,c 75.9 72.4 72.6 72.3 72.4 84.8 69.2 0 0 33.01 0.7654 32.96 0.7614 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

5a,b,c 74.8 72.5 72.7 72.4 72.5 85.5 69.2 0 0 34.04 0.7891 34.03 0.7859 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

6a,b,c 75 72.4 72.5 72.2 72.4 86.6 69.2 0 0 35.06 0.8124 35.22 0.8133 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

7a,b,c 75.6 72.4 72.6 72.3 72.4 87.6 69.2 0 0 36.05 0.8353 36.12 0.8336 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

8a,b,c 75.5 72.4 72.6 72.3 72.4 88.2 69.2 0 0 37.1 0.8601 37.14 0.8569 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

9a,b,c 75.9 72.5 72.7 72.4 72.4 89.3 69.2 0 0 38.15 0.8836 38.14 0.8798 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

10a,b,c 75.9 72.8 72.9 72.7 72.6 90.7 69.2 0 0 39.16 0.9072 39.23 0.9049 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

11a,b,c 75.4 72.7 72.9 72.7 72.6 91.2 69.2 0 0 40.07 0.9275 40.12 0.9248 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

12a,b,c 74.9 72.9 73 72.9 72.8 92.2 69.2 0 0 41.01 0.9498 41.26 0.9514 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

13a,b,c 75.8 72.9 73 72.8 72.7 93.4 69.2 0 0 42.1 0.9737 42.11 0.9706 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

14a,b,c 75.6 72.9 73 72.8 72.8 94.7 69.2 0 0 43.08 0.9966 43.07 0.9923 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

15a,b,c 76.1 72.9 73 72.8 72.8 95.6 69.2 0 0 44.05 1.0192 44.3 1.0203 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

16a,b,c 75.4 72.9 73 72.9 72.8 96.1 69.2 0 0 45.07 1.0424 45.01 1.0369 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

17a,b,c 76.3 73 73.1 72.9 72.9 97.5 69.2 0 0 46.05 1.0651 46.25 1.0645 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

18a,b,c 76.3 73 73.1 72.9 72.8 99 69.2 0 0 47.11 1.0891 47.01 1.0818 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

19a,b,c 75.6 72.8 73 72.8 72.8 99.7 69.2 0 0 48.22 1.1132 48.09 1.1066 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

20a,b,c 75.7 72.7 72.8 72.8 72.9 101.1 69.2 0 0 49.26 1.1382 49.09 1.1297 orange 11.02 10.23 10.54 10.59 5.6 5.6 0 29.95

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -23

11crossover holes-9 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 5 degree 11 cross-over holes---9 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 03 / 30 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 72.4 71.7 71.9 72 0.284 0.259 0.274 0.274 0.173 0.204 water 29.76 0.015 71.5 0

10 72.4 71.7 71.9 72 0.46 0.431 0.431 0.445 0.273 0.325 water 29.76 0.021 71.5 0

15 72.4 71.7 71.9 72 0.627 0.614 0.619 0.626 0.398 0.464 water 29.76 0.033 71.5 0

20 72.4 71.7 71.9 72 0.849 0.795 0.817 0.826 0.532 0.612 water 29.76 0.039 71.5 0

25 72.4 71.7 71.9 72 2.7 2.56 2.59 2.62 1.65 1.95 orange 29.76 0.15 71.5 0

30 72.4 71.7 71.9 72 3.43 3.25 3.31 3.31 2.09 2.47 orange 29.76 0.2 71.5 0

40 72.4 71.7 71.9 72 4.86 4.61 4.7 4.72 2.95 3.51 orange 29.76 0.26 71.5 0

50 72.4 71.7 71.9 72 6.94 6.55 6.69 6.76 4.21 5 orange 29.76 0.38 71.5 0

60 72.4 71.7 71.9 72 9.18 8.69 8.82 8.91 5.58 6.61 orange 29.76 0.52 71.5 0

70 72.4 71.7 71.9 72 11.52 10.93 11.16 11.2 6.99 8.35 orange 29.76 0.69 71.5 0

80 72.4 71.7 71.9 72 14.03 13.21 13.57 13.57 8.49 10.13 orange 29.76 0.83 71.5 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11-9exit(3blocked)

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/28/2012

13 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.4 71.7 71.9 71.7 72.7 77.5 72 0 0 21.73 0.504 21.78 0.5038 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

2a,b,c 71.9 71.6 71.8 71.5 72.6 78.5 72 0 0 22.35 0.5186 22.34 0.5166 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

3a,b,c 71.8 71.5 71.8 71.5 72.5 79.5 72 0 0 22.94 0.5325 22.87 0.5288 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

4a,b,c 72 71.5 71.8 71.5 72.4 79.6 72 0 0 23.34 0.5418 23.41 0.5413 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

5a,b,c 71.6 71.4 71.6 71.3 72.2 80.5 72 0 0 23.97 0.556 23.97 0.5541 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

6a,b,c 71.7 71.3 71.6 71.3 72.1 80.9 72 0 0 24.61 0.571 24.58 0.568 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

7a,b,c 71.3 71.4 71.6 71.3 72.1 81.3 72 0 0 25.18 0.5841 25.12 0.586 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

8a,b,c 71.8 71.2 71.5 71.2 72 81.8 72 0 0 25.81 0.5986 25.78 0.5957 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

9a,b,c 71.2 71.1 71.3 71.2 71.9 82.6 72 0 0 26.49 0.6145 26.56 0.6134 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

10a,b,c 70.8 71.1 71.4 71.1 71.9 83.2 72 0 0 27.2 0.631 27.22 0.629 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

11a,b,c 71.5 71.1 71.3 71.2 71.9 83.9 72 0 0 27.77 0.6439 27.9 0.6445 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

12a,b,c 70.5 70.9 71.1 70.9 71.8 84.7 72 0 0 28.6 0.6608 28.6 0.6613 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

13a,b,c 70.7 70.9 71.1 70.9 71.7 85.2 72 0 0 29.35 0.6802 29.4 0.6785 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

14a,b,c 70.5 70.9 71.1 71 71.6 85.7 72 0 0 30.07 0.6965 30.03 0.9634 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

15a,b,c 70.5 70.9 71.1 70.9 71.7 86.7 72 0 0 30.8 0.7137 30.72 0.7091 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

16a,b,c 70.4 70.9 71.1 70.9 71.7 87.4 72 0 0 31.38 0.727 31.41 0.7247 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

17a,b,c 70.7 70.7 70.9 70.7 71.6 88.2 72 0 0 32.11 0.7438 32.07 0.7397 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

18a,b,c 70.9 70.7 70.9 70.7 71.6 88.8 72 0 0 32.7 0.7572 32.78 0.7566 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

19a,b,c 70.1 70.7 70.9 70.7 71.6 90 72 0 0 33.4 0.7738 33.45 0.7717 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

20a,b,c 70.7 70.6 70.8 70.6 71.6 90.8 72 0 0 34.19 0.7913 34.22 0.7888 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

21a,b,c 70.9 70.7 70.9 70.7 71.7 91.7 72 0 0 35.19 0.8158 35.15 0.8116 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

22a,b,c 71.6 70.9 71.1 70.9 71.8 92.6 72 0 0 36.17 0.8384 36.2 0.8357 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

23a,b,c 71.2 70.9 71.1 70.8 71.8 94.6 72 0 0 37.11 0.8601 37.13 0.857 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

24a,b,c 71.2 70.8 71 70.9 71.7 95.3 72 0 0 38.05 0.8816 38.1 0.8792 water 0.563 0.529 0.54 0.541 0.341 0.403 0.028 29.76

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -24

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/28/2012

26 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.8 70.1 70.3 70.1 71.2 75.7 72.4 0 0 22.8 0.5293 22.92 0.5303 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

2a,b,c 69.7 69.9 70.2 69.9 71.1 76.2 72.4 0 0 23.56 0.5468 23.61 0.5461 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

3a,b,c 70.2 70 70.2 70 71.1 76.8 72.4 0 0 24.27 0.5631 24.31 0.5615 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

4a,b,c 71.1 70 70.3 70 71.1 77.3 72.4 0 0 25.03 0.5809 25 0.5781 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

5a,b,c 71 70.2 70.3 70.1 71.1 77.8 72.4 0 0 25.81 0.5987 25.79 0.5963 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

6a,b,c 71.9 70.3 70.4 70.2 71.1 78.3 72.4 0 0 26.41 0.6126 26.49 0.6126 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

7a,b,c 71.2 70.4 70.5 70.3 71.1 78.8 72.4 0 0 27.07 0.6279 27.16 0.6276 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

8a,b,c 71.3 70.5 70.6 70.4 71.1 79.4 72.4 0 0 27.86 0.6462 27.89 0.6444 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

9a,b,c 71.6 70.6 70.7 70.5 71.1 80 72.4 0 0 28.5 0.661 28.58 0.6604 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

10a,b,c 71.3 70.6 70.8 70.5 71.1 80.5 72.4 0 0 29.3 0.6938 29.29 0.6761 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

11a,b,c 71.3 70.6 70.8 70.5 71.1 81.1 72.4 0 0 29.93 0.7126 29.98 0.6927 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

12a,b,c 71.3 70.6 70.8 70.5 71.2 81.5 72.4 0 0 30.75 0.7297 30.75 0.7101 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

13a,b,c 71.1 70.6 70.8 70.6 71.2 82.1 72.4 0 0 31.49 0.7438 31.42 0.7261 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

14a,b,c 71.1 70.6 70.8 70.5 71.2 82.8 72.4 0 0 32.1 0.7649 32.2 0.7443 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

15a,b,c 71.2 70.4 70.8 70.6 71.2 83.2 72.4 0 0 33.01 0.7842 33.06 0.7627 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

16a,b,c 71.3 70.5 70.6 70.3 71.1 83.8 72.4 0 0 33.86 0.8078 33.76 0.7788 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

17a,b,c 70.6 70.5 70.7 70.5 71.1 84.7 72.4 0 0 34.89 0.8293 34.95 0.8064 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

18a,b,c 70.7 70.5 70.7 70.5 71.1 85.1 72.4 0 0 35.84 0.8517 35.84 0.8265 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

19a,b,c 71 70.5 70.7 70.5 71.1 86.1 72.4 0 0 36.8 0.8799 36.87 0.8501 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

20a,b,c 70.5 70.5 70.7 70.4 71.1 86.8 72.4 0 0 38.01 0.924 37.93 0.873 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

21a,b,c 71.8 71 71.1 70.9 71.6 87.7 72.4 0 0 39.13 0.9073 39.2 0.9054 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

22a,b,c 71.7 71 71.2 71 71.7 89.1 72.4 0 0 40.31 0.9343 40.33 0.9313 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

23a,b,c 72.1 71 71.2 71 71.7 90.2 72.4 0 0 41.43 0.9603 41.47 0.9572 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

24a,b,c 71.9 71 71.2 71 71.7 91.6 72.4 0 0 42.52 0.9851 42.5 0.9807 orange 2.7 2.56 2.59 2.62 1.65 1.95 0.15 29.68

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:03/28/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.4 70.4 70.6 70.4 71.1 75.2 69.0 0 0 24.17 0.5605 24.07 0.5576 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

2a,b,c 71.8 70.4 70.6 70.4 71.1 75.9 69.0 0 0 25.00 0.5802 25.10 0.5804 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

3a,b,c 72.1 70.5 70.8 70.5 71.2 76.5 69.0 0 0 26.06 0.6048 26.17 0.6052 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

4a,b,c 72.6 70.7 70.9 70.6 71.2 77.0 69.0 0 0 27.07 0.6277 27.13 0.6268 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

5a,b,c 72.3 70.7 70.9 70.7 71.2 77.5 69.0 0 0 28.03 0.6505 28.13 0.6499 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

6a,b,c 71.9 70.8 70.9 70.7 71.2 77.9 69.0 0 0 28.82 0.6686 28.88 0.6683 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

7a,b,c 72.1 70.9 71.0 70.8 71.3 78.4 69.0 0 0 29.69 0.6885 29.75 0.6871 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

8a,b,c 72.0 70.9 71.0 70.8 71.3 78.9 69.0 0 0 30.76 0.7135 30.79 0.7113 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

9a,b,c 72.0 70.8 71.0 70.8 71.3 79.3 69.0 0 0 31.76 0.7362 31.70 0.7321 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

10a,b,c 72.1 70.8 70.9 70.7 71.2 79.8 69.0 0 0 32.61 0.7556 32.46 0.7496 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

11a,b,c 71.6 70.8 70.9 70.7 71.2 80.2 69.0 0 0 33.35 0.7726 33.33 0.7697 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

12a,b,c 72.1 70.7 70.9 70.7 71.2 80.9 69.0 0 0 34.04 0.7887 34.17 0.7889 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

13a,b,c 71.4 70.7 70.9 70.7 71.2 81.4 69.0 0 0 35.15 0.8141 35.23 0.8132 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

14a,b,c 71.7 70.7 70.9 70.7 71.2 82.0 69.0 0 0 36.23 0.8383 36.25 0.8367 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

15a,b,c 71.2 70.5 70.7 70.4 71.1 82.5 69.0 0 0 37.31 0.8637 37.21 0.8581 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

16a,b,c 71.4 70.5 70.7 70.4 71.1 83.2 69.0 0 0 38.32 0.8870 28.25 0.8828 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

17a,b,c 70.8 70.4 70.7 70.4 71.1 83.8 69.0 0 0 39.30 0.9092 39.32 0.9067 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

18a,b,c 71.2 70.4 70.6 70.4 71.1 84.5 69.0 0 0 40.39 0.9340 40.34 0.9303 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

19a,b,c 71.4 70.4 70.6 70.4 71.1 85.3 69.0 0 0 41.18 0.9530 41.32 0.9521 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

20a,b,c 70.9 70.4 70.6 70.4 71.1 85.9 69.0 0 0 42.27 0.9775 42.32 0.9755 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

21a,b,c 72.6 71.2 71.4 71.1 71.6 86.2 69 0 0 43.49 1.0079 43.76 0.9992 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

22a,b,c, 72.6 71.4 71.5 71.3 71.7 87.6 69 0 0 44.63 1.0341 44.64 1.0305 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

23a,b,c 72.7 71.3 71.4 71.3 71.7 89.1 69 0 0 45.93 1.0639 45.91 1.0594 orange 4.86 4.61 4.7 4.72 2.95 3.51 0.26 29.63

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -25

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:03/28/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.9 70.0 70.1 49.9 70.4 74.4 70.2 0 0 25.25 0.5860 25.30 0.5851 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

2a,b,c 72.8 70.1 70.2 70.1 70.4 74.8 70.2 0 0 26.26 0.6092 26.30 0.6082 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

3a,b,c 73.9 70.6 70.6 70.4 70.6 75.6 70.2 0 0 27.35 0.6345 27.38 0.6333 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

4a,b,c 73.1 70.6 70.7 70.5 70.6 76.1 70.2 0 0 28.35 0.6575 28.43 0.6570 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

5a,b,c 73.2 70.8 70.9 70.7 70.7 76.7 70.2 0 0 29.38 0.6814 29.36 0.6785 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

6a,b,c 73.3 70.9 71.0 70.8 70.8 77.2 70.2 0 0 30.37 0.7043 30.43 0.7029 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

7a,b,c 73.6 71.1 71.2 71.0 70.9 77.9 70.2 0 0 31.45 0.7291 31.39 0.7256 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

8a,b,c 73.3 71.4 71.5 71.2 71.2 78.6 70.2 0 0 32.31 0.7491 32.51 0.7511 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

9a,b,c 73.4 71.5 71.6 71.4 71.3 79.1 70.2 0 0 33.43 0.7744 33.28 0.7687 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

10a,b,c 73.5 71.7 71.8 71.6 71.5 79.8 70.2 0 0 34.34 0.7950 34.22 0.7900 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

11a,b,c 73.8 71.7 71.8 71.6 71.6 80.3 70.2 0 0 35.22 0.8158 35.26 0.8139 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

12a,b,c 73.9 71.7 71.8 71.6 71.6 80.8 70.2 0 0 36.30 0.8408 36.38 0.8399 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

13a,b,c 73.3 71.6 71.7 71.5 71.6 81.3 70.2 0 0 37.51 0.8682 37.50 0.8652 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

14a,b,c 73.3 71.4 71.6 71.3 71.6 82.1 70.2 0 0 38.46 0.8902 38.47 0.8874 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

15a,b,c 72.9 71.5 71.7 71.4 71.7 82.5 70.2 0 0 39.40 0.9123 39.44 0.9091 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

16a,b,c 72.9 71.7 71.8 71.6 71.7 83.2 70.2 0 0 40.44 0.9356 40.27 0.9283 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

17a,b,c 72.9 71.7 71.8 71.7 71.8 84.0 70.2 0 0 41.44 0.9587 41.46 0.9564 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

18a,b,c 73.2 71.7 71.9 71.6 71.9 84.6 70.2 0 0 42.42 0.9815 42.59 0.9810 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

19a,b,c 73.4 71.8 71.9 71.7 72.0 85.3 70.2 0 0 43.75 1.0117 43.88 1.0110 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

20a,b,c 72.9 71.8 71.8 71.7 71.9 85.9 70.2 0 0 44.68 1.0314 44.76 1.0312 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

21a,b,c 73.8 71.6 71.7 71.5 71.8 86.5 70.2 0 0 46.03 1.0667 45.88 1.0599 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

22a,b,c 74.1 71.7 71.8 71.6 71.9 87.1 70.2 0 0 47.10 1.0910 47.11 1.0875 orange 6.69 6.31 6.49 6.53 4.11 4.84 0.39 29.58

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:03/28/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.8 71.9 72.5 71.8 72.0 75.5 71.4 0 0 26.71 0.6198 26.59 0.6151 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

2a,b,c 75.6 72.5 72.5 72.4 72.0 76.3 71.4 0 0 27.63 0.6411 27.70 0.6406 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

3a,b,c 75.1 72.5 72.5 72.4 72.0 76.8 71.4 0 0 28.65 0.6639 28.71 0.6639 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

4a,b,c 74.4 72.5 72.5 72.4 72.0 77.1 71.4 0 0 29.77 0.6903 29.77 0.6881 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

5a,b,c 74.6 72.5 72.5 72.4 72.0 77.6 71.4 0 0 30.69 0.7116 30.75 0.7108 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

6a,b,c 74.9 71.9 72.1 71.9 72.0 77.9 71.4 0 0 31.67 0.7341 31.74 0.7336 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

7a,b,c 74.3 71.9 72.1 71.9 72.0 78.2 71.4 0 0 32.75 0.7593 32.81 0.7580 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

8a,b,c 73.8 71.9 72.1 71.9 72.0 78.5 71.4 0 0 33.62 0.7790 33.64 0.7767 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

9a,b,c 74.6 71.9 72.1 71.9 72.0 78.9 71.4 0 0 34.70 0.8039 34.80 0.8036 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

10a,b,c 74.6 71.9 72.1 71.9 72.0 79.2 71.4 0 0 35.75 0.8286 35.84 0.8276 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

11a,b,c 74.4 71.9 72.1 71.7 72.0 79.6 71.4 0 0 36.68 0.8496 36.77 0.8491 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

12a,b,c 73.5 71.9 72.1 71.7 72.0 79.9 71.4 0 0 37.60 0.8720 37.69 0.8704 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

13a,b,c 74.4 71.9 72.1 71.7 72.0 80.4 71.4 0 0 38.72 0.8966 38.71 0.8932 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

14a,b,c 74.3 71.9 72.1 71.7 72.0 80.8 71.4 0 0 39.60 0.9169 39.77 0.9177 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

15a,b,c 74.3 71.9 72.1 71.7 72.0 81.2 71.4 0 0 40.81 0.9449 40.69 0.9390 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

16a,b,c 74.1 71.9 72.1 71.7 72.0 81.6 71.4 0 0 41.61 0.9628 41.69 0.9613 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

17a,b,c 73.4 71.9 72.1 71.7 72.0 82.1 71.4 0 0 42.78 0.9902 42.68 0.9841 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

18a,b,c 73.6 71.9 72.1 71.7 72.0 82.7 71.4 0 0 43.72 1.0112 43.86 1.0106 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

19a,b,c 73.4 71.9 72.1 71.7 72.0 83.4 71.4 0 0 45.03 1.0414 45.09 1.0387 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

20a,b,c 74.2 71.9 72.1 71.7 72.0 83.9 71.4 0 0 46.47 1.0741 46.39 1.0677 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

21a,b,c 74.6 71.9 72.1 71.8 72 84.1 71.4 0 0 47.23 1.0948 47.17 1.0895 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

22a,b,c 74.2 71.9 72.1 71.8 72 84.7 71.4 0 0 48.27 1.1183 48.28 1.1151 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

23a,b,c 73.9 71.9 72.1 71.8 72 85.4 71.4 0 0 49.45 1.1453 49.56 1.1441 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

24a,b,c 74.9 71.9 72.1 71.8 72 86.1 71.4 0 0 50.73 1.1746 50.68 1.1694 orange 11.250 10.670 10.900 10.950 6.836 8.110 0.640 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -26

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:03/30/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.6 71.6 71.9 71.7 72.0 74.5 71.4 0 0 27.11 0.6276 27.04 0.6242 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

2a,b,c 74.6 71.6 71.9 71.7 72.0 75.4 71.4 0 0 28.27 0.6548 28.27 0.6538 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

3a,b,c 74.6 71.6 71.9 71.7 72.0 76.1 71.4 0 0 29.52 0.6865 29.51 0.6852 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

4a,b,c 74.6 71.6 71.9 71.7 72.0 76.6 71.4 0 0 30.78 0.7162 30.86 0.7160 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

5a,b,c 74.6 71.6 71.9 71.7 72.0 77.0 71.4 0 0 32.11 0.7463 31.94 0.7412 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

6a,b,c 73.8 71.6 71.9 71.7 72.0 77.4 71.4 0 0 33.33 0.7745 33.32 0.7729 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

7a,b,c 73.8 71.6 71.9 71.7 72.0 77.8 71.4 0 0 34.57 0.8031 34.50 0.8002 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

8a,b,c 73.8 71.6 71.9 71.7 72.0 78.2 71.4 0 0 35.86 0.8332 35.85 0.8314 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

9a,b,c 73.8 71.6 71.9 71.7 72.0 78.7 71.4 0 0 37.14 0.8623 37.12 0.8602 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

10a,b,c 73.8 71.6 71.9 71.7 72.0 79.1 71.4 0 0 38.13 0.8556 38.21 0.8865 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

11a,b,c 73.8 71.2 71.7 71.3 72.0 79.4 71.4 0 0 39.37 0.9135 39.34 0.9125 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

12a,b,c 73.8 71.2 71.7 71.3 72.0 79.7 71.4 0 0 40.56 0.9415 40.42 0.9365 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

13a,b,c 73.8 71.2 71.7 71.3 72.0 80.2 71.4 0 0 41.56 0.9641 41.38 0.9580 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

14a,b,c 73.8 71.2 71.7 71.3 72.0 80.5 71.4 0 0 42.41 0.9831 42.53 0.9840 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

15a,b,c 73.8 71.2 71.7 71.3 72.0 81.1 71.4 0 0 43.43 1.0071 43.65 1.0116 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

16a,b,c 73.8 71.2 71.7 71.3 72.0 81.5 71.4 0 0 44.80 1.0381 44.87 1.0379 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

17a,b,c 73.8 71.2 71.7 71.3 72.0 82.1 71.4 0 0 46.14 1.0685 46.10 1.0667 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

18a,b,c 73.8 71.2 71.7 71.3 72.0 82.7 71.4 0 0 47.78 1.1067 47.46 1.0972 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

19a,b,c 73.8 71.2 71.7 71.3 72.0 83.1 71.4 0 0 48.83 1.1300 48.91 1.1300 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

20a,b,c 73.8 71.2 71.7 71.3 72.0 84.0 71.4 0 0 50.56 1.1690 50.52 1.1670 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

21a,b,c 74.1 71.2 72 71.9 72 85.0 71.4 0 0 51.43 1.1917 51.47 1.1890 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

22a,b,c 74.7 71.2 72 71.1 72 85.6 71.4 0 0 52.57 1.2172 52.65 1.2152 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

23a,b,c 75.0 71.2 72 70.5 72 86.0 71.4 0 0 53.67 1.2425 53.69 1.2386 orange 14.03 13.21 13.57 13.57 8.49 10.13 0.83 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -27

11crossover holes-8 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 5 degree 11 cross-over holes---8 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 08 /2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 70.4 71 71.3 70.5 0.349 0.33 0.33 0.337 0.216 0.274 water 29.98 0.022 71 0

10 70.5 71 71.1 70.5 0.551 0.525 0.532 0.537 0.361 0.446 water 29.98 0.033 71 0

15 70.5 70.7 70.9 70.5 0.77 0.753 0.76 0.766 0.515 0.631 water 29.98 0.047 70.7 0

20 70.3 70.5 70.8 70.5 2.63 2.49 2.55 2.54 0.693 0.85 water/orange 29.98 0.066 70.5 0

25 70.3 70.4 70.6 70.5 3.35 3.21 3.25 3.29 2.21 2.71 orange 29.98 0.22 70.4 0

30 70.6 70.4 70.6 70.5 4.19 4.01 4.09 4.09 2.78 3.47 orange 29.98 0.22 70.4 0

40 71.5 70.4 70.6 70.5 6.12 5.84 5.96 5.99 4.03 4.94 orange 29.98 0.36 70.4 0

50 71.7 70.5 70.7 70.5 8.42 8.06 8.19 8.21 5.56 6.79 orange 29.98 0.5 70.4 0

60 71.7 70.5 70.7 70.5 10.94 10.49 10.63 10.71 7.21 8.85 orange 29.98 0.64 70.4 0

70 71.7 70.5 70.7 70.5 13.9 13.25 13.54 13.61 9.1 11.21 orange 29.98 0.86 70.4 0

80 71.7 70.5 70.7 70.5 17.17 16.45 16.59 16.85 11.23 13.94 orange 29.98 0.99 70.4 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11-8exit(4blocked)

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:4/6/2012

13 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.7 71.4 71.7 71.3 72.6 78.4 70.7 0 0 20.56 0.4769 20.54 0.4753 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

2a,b,c 71.2 71.1 71.5 71 72.4 78.8 70.7 0 0 21.27 0.4933 21.13 0.4893 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

3a,b,c 71 71.1 71.4 71.1 72.3 79.1 70.7 0 0 21.77 0.5048 21.79 0.5043 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

4a,b,c 70.7 71.1 71.4 71 72.3 79.5 70.7 0 0 22.4 0.5196 22.36 0.5173 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

5a,b,c 70.8 71.1 71.3 71 72.1 80 70.7 0 0 22.89 0.5309 22.97 0.5315 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

6a,b,c 70.6 70.9 71.1 70.9 71.9 80.4 70.7 0 0 23.64 0.548 23.54 0.5443 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

7a,b,c 70.7 70.9 71.1 70.9 71.8 80.9 70.7 0 0 24.14 0.5599 24.15 0.5588 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

8a,b,c 70.5 70.9 71 70.9 71.7 81.5 70.7 0 0 24.94 0.5783 24.88 0.5757 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

9a,b,c 71.2 70.8 71 70.7 71.7 82 70.7 0 0 25.45 0.5902 25.44 0.5885 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

10a,b,c 70.3 70.7 71 70.7 71.7 82.6 70.7 0 0 26.11 0.6051 26.04 0.6022 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

11a,b,c 70.1 70.6 70.9 70.6 71.6 83.2 70.7 0 0 26.76 0.6204 26.71 0.6186 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

12a,b,c 70.1 70.5 70.8 70.5 71.5 84 70.7 0 0 27.63 0.6406 27.48 0.635 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

13a,b,c 70.1 70.6 70.7 70.6 71.4 84.6 70.7 0 0 28.2 0.6539 28.16 0.6509 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

14a,b,c 70.7 70.4 70.6 70.5 71.3 85.5 70.7 0 0 28.86 0.6694 28.87 0.6669 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

15a,b,c 69.9 70.4 70.6 70.4 71.4 86.3 70.7 0 0 29.61 0.6863 29.65 0.6853 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

16a,b,c 70.5 70.4 70.6 70.3 71.3 87 70.7 0 0 30.31 0.7025 30.2 0.6978 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

17a,b,c 69.8 70.4 70.7 70.4 71.4 87.9 70.7 0 0 31 0.7183 31.01 0.7171 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

18a,b,c 70.1 70.2 70.5 70.2 71.3 88.5 70.7 0 0 31.63 0.733 31.71 0.7331 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

19a,b,c 69.7 70.2 70.5 70.2 71.2 89.3 70.7 0 0 32.4 0.7508 32.34 0.747 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

20a,b,c 69.8 70.1 70.4 70.2 71.2 90.1 70.7 0 0 33.1 0.7666 33.14 0.7642 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

21a,b,c 70.2 70.1 70.4 70.1 71.2 91.1 70.7 0 0 33.78 0.7827 33.71 0.7786 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

22a,b,c 69.7 70.2 70.3 70.3 71.1 91.8 70.7 0 0 34.41 0.7962 34.43 0.795 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

23a,b,c 70 70.3 70.5 70.3 71.3 93.3 70.7 0 0 35.13 0.8137 35.22 0.8127 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

24a,b,c 69.6 70.2 70.5 70.3 71.3 94.8 70.7 0 0 36.16 0.8375 36.12 0.8334 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

25a,b,c 69.5 70.1 70.4 70.1 71.2 95.6 70.7 0 0 36.83 0.8515 36.88 0.8504 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

26a,b,c 69.7 70.2 70.4 70.2 71.3 96.8 70.7 0 0 37.57 0.87 37.49 0.8654 water 0.697 0.654 0.662 0.671 0.456 0.556 0.04 29.88

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -28

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

26 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.2 69.8 70.1 69.8 70.8 75.3 70.9 0 0 22 0.5105 22.01 0.5098 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

2a,b,c 69.4 69.8 70 69.7 70.8 75.8 70.9 0 0 22.89 0.5311 22.93 0.5309 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

3a,b,c 69.3 69.7 70 69.7 70.8 76.3 70.9 0 0 23.74 0.551 23.79 0.5508 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

4a,b,c 69.3 69.7 70 69.7 70.8 76.8 70.9 0 0 24.62 0.5712 24.66 0.5708 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

5a,b,c 69.4 69.7 70 69.7 70.7 77.4 70.9 0 0 25.43 0.59 25.47 0.5896 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

6a,b,c 69.2 69.6 69.8 69.5 70.6 77.8 70.9 0 0 26.21 0.6081 26.32 0.6092 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

7a,b,c 70.1 69.6 69.9 69.6 70.6 78.4 70.9 0 0 27.04 0.6272 27.13 0.628 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

8a,b,c 70.2 69.6 69.9 69.6 70.6 78.8 70.9 0 0 27.84 0.6457 27.85 0.6445 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

9a,b,c 69.4 69.7 69.9 69.7 70.7 79.5 70.9 0 0 28.62 0.6652 28.61 0.662 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

10a,b,c 69.9 69.7 70 69.7 70.7 80 70.9 0 0 29.48 0.6839 29.51 0.6829 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

11a,b,c 69.5 69.7 70 69.7 70.7 80.7 70.9 0 0 30.41 0.7052 30.42 0.7043 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

12a,b,c 69.4 69.6 70.6 69.6 70.6 81.3 70.9 0 0 31.35 0.7268 31.37 0.7255 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

13a,b,c 69.3 69.6 70.6 69.6 70.6 81.9 70.9 0 0 32.21 0.7467 32.15 0.7433 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

14a,b,c 69.4 69.6 70.6 69.6 70.6 82.7 70.9 0 0 33.07 0.7658 33.06 0.7644 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

15a,b,c 70 69.6 70.6 69.6 70.6 83.6 70.9 0 0 34.03 0.7886 33.93 0.7843 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

16a,b,c 69.4 69.7 70.7 69.6 70.7 84.2 70.9 0 0 35 0.811 34.9 0.8066 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

17a,b,c 69.7 69.8 70.8 69.8 70.8 85 70.9 0 0 35.82 0.8299 35.85 0.8281 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

18a,b,c 70.5 69.8 70.7 69.8 70.7 86.1 70.9 0 0 37.03 0.8575 36.85 0.8503 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

19a,b,c 70.4 69.8 70.6 69.7 70.6 86.9 70.9 0 0 38.05 0.8813 38.06 0.8789 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

20a,b,c 69.4 69.6 70.6 69.6 70.6 88.2 70.9 0 0 39.06 0.9044 39.07 0.9022 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

21a,b,c 70.3 69.7 70.6 69.6 70.6 88.6 70.9 0 0 40.12 0.9291 40.12 0.926 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

22a,b,c 69.5 69.7 70.6 69.6 70.6 90 70.9 0 0 41.05 0.9501 41.07 0.9478 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

23a,b,c 69.5 69.7 70.7 69.7 70.7 90.8 70.9 0 0 42.09 0.974 42.08 0.9704 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

24a,b,c 70.1 69.7 70.7 69.7 70.7 91.6 70.9 0 0 43.2 0.9995 43.18 0.9959 orange 3.5 3.35 3.42 3.43 2.32 2.85 0.23 29.89

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/07/2012

40 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.8 71.9 72.2 71.8 72.2 76.3 71.2 0 0 23.57 0.5469 23.61 0.5469 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

2a,b,c 73.1 71.8 72 71.7 72 77 71.2 0 0 24.79 0.5753 24.78 0.5737 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

3a,b,c 72.7 71.7 71.9 71.6 71.9 77.6 71.2 0 0 26.14 0.6065 26.11 0.6045 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

4a,b,c 72.5 71.6 71.9 71.5 71.9 78.1 71.2 0 0 27.31 0.6336 27.29 0.6318 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

5a,b,c 72.3 71.5 71.7 71.4 71.7 78.6 71.2 0 0 28.48 0.6607 28.42 0.6577 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

6a,b,c 72.9 71.3 71.6 71.3 71.6 78.9 71.2 0 0 29.52 0.6846 29.51 0.6832 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

7a,b,c 72.2 71.2 71.5 71.2 71.5 79.5 71.2 0 0 30.6 0.7079 30.63 0.709 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

8a,b,c 72.4 71.2 71.4 71.1 71.4 80.1 71.2 0 0 31.67 0.7345 31.79 0.7355 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

9a,b,c 72.6 71 71.3 71 71.3 80.8 71.2 0 0 32.86 0.7618 32.86 0.7603 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

10a,b,c 72.1 70.9 71.2 70.9 71.2 81.2 71.2 0 0 33.97 0.7876 33.98 0.786 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

11a,b,c 71.8 70.8 71 70.9 71 82 71.2 0 0 35.24 0.8169 35.26 0.815 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

12a,b,c 72.1 70.9 71.1 70.8 71.1 82.7 71.2 0 0 36.23 0.8396 36.22 0.8373 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

13a,b,c 71.1 70.6 70.9 70.6 70.9 83.2 71.2 0 0 37.49 0.8688 37.43 0.8652 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

14a,b,c 71.1 70.5 70.7 70.4 70.7 83.8 71.2 0 0 38.68 0.8961 38.65 0.893 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

15a,b,c 71.3 70.5 70.7 70.4 70.7 84.8 71.2 0 0 39.59 0.9171 39.56 0.9141 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

16a,b,c 71.1 70.4 70.6 70.4 70.6 85.5 71.2 0 0 40.62 0.9407 40.55 0.9365 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

17a,b,c 70.5 70.4 70.6 70.3 70.6 86.1 71.2 0 0 41.57 0.9625 41.65 0.9618 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

18a,b,c 71.2 70.4 70.6 70.3 70.6 86.8 71.2 0 0 42.49 0.9835 42.5 0.9815 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

19a,b,c 71.2 70.3 70.5 70.3 70.5 87.4 71.2 0 0 43.59 1.0088 43.7 1.0088 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

20a,b,c 70.4 70.2 70.4 70.2 70.4 88.3 71.2 0 0 44.73 1.0352 44.83 1.0344 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

21a,b,c 71.1 70.1 70.4 70.1 70.4 88.9 71.2 0 0 45.67 1.0567 45.63 1.0527 orange 6.12 5.84 5.96 5.99 4.03 4.94 0.36 29.92

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -29

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/07/2012

54 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.8 71.4 71.6 71.3 71.5 75 71.1 0 0 24.51 0.5687 24.58 0.5693 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

2a,b,c 74.1 71.6 71.8 71.5 71.6 75.8 71.1 0 0 25.54 0.5927 25.55 0.5917 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

3a,b,c 73.8 71.7 71.9 71.6 71.7 76.3 71.1 0 0 26.65 0.6185 26.58 0.6153 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

4a,b,c 73.8 71.8 71.9 71.6 71.8 76.8 71.1 0 0 27.6 0.6404 27.65 0.6404 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

5a,b,c 73.9 71.8 72 71.7 71.8 77.2 71.1 0 0 28.53 0.662 28.62 0.6626 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

6a,b,c 73.9 71.7 71.8 71.6 71.8 77.7 71.1 0 0 29.59 0.6863 29.6 0.6853 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

7a,b,c 73.5 71.4 71.7 71.3 71.7 78.1 71.1 0 0 30.59 0.7096 30.59 0.7081 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

8a,b,c 72.9 71.4 71.6 71.3 71.7 78.5 71.1 0 0 31.55 0.7318 31.65 0.7326 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

9a,b,c 72.2 71.2 71.4 71.1 71.6 78.9 71.1 0 0 32.66 0.7575 32.67 0.756 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

10a,b,c 72.3 71.1 71.3 71.1 71.5 79.3 71.1 0 0 33.52 0.7774 33.62 0.7778 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

11a,b,c 72.1 71 71.2 70.9 71.5 79.7 71.1 0 0 34.59 0.8022 34.48 0.7976 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

12a,b,c 71.6 70.9 71.2 70.8 71.5 80.2 71.1 0 0 35.63 0.8262 35.61 0.8237 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

13a,b,c 71.5 70.9 71.1 70.8 71.4 80.6 71.1 0 0 36.57 0.8476 36.54 0.8454 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

14a,b,c 72.6 71 71.2 71 71.6 81.1 71.1 0 0 37.69 0.8735 37.59 0.8693 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

15a,b,c 72.6 70.9 71.1 70.9 71.5 81.8 71.1 0 0 38.6 0.8943 38.59 0.8922 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

16a,b,c 71.5 70.9 71 70.9 71.4 82.2 71.1 0 0 39.56 0.9165 39.58 0.915 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

17a,b,c 72.2 70.9 71.1 70.8 71.5 82.8 71.1 0 0 40.6 0.9406 40.51 0.9362 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

18a,b,c 71.2 70.7 70.8 70.6 71.4 83.1 71.1 0 0 41.56 0.9625 41.51 0.959 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

19a,b,c 72.1 70.5 70.8 70.5 71.3 83.6 71.1 0 0 42.51 0.9843 42.54 0.983 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

20a,b,c 72.1 70.4 70.6 70.4 71.2 84.3 71.1 0 0 43.57 1.0088 43.56 1.0062 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

21a,b,c 72.3 70.4 70.6 70.4 71.2 84.8 71.1 0 0 44.57 1.3017 44.69 1.0319 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

22a,b,c 71.9 70.5 70.7 70.4 71.2 85.5 71.1 0 0 45.65 1.0567 45.74 1.0559 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

23a,b,c 72.2 70.5 70.7 70.5 71.2 86.4 71.1 0 0 47.03 1.0881 47.02 1.0852 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

24a,b,c 72.9 70.7 71 70.7 71.4 87.3 71.1 0 0 48.01 1.1106 48.15 1.111 orange 9.34 8.97 9.11 9.18 6.16 7.59 0.58 29.93

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/07/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.1 72.2 72.3 72 72.2 75.5 71.1 0 0 25.16 0.5838 25.19 0.5838 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

2a,b,c 76.1 72.3 72.4 72.3 72.2 76 71.1 0 0 26.34 0.6111 26.35 0.6103 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

3a,b,c 75.7 72.4 72.5 72.3 72.3 76.5 71.1 0 0 27.52 0.6387 27.51 0.6371 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

4a,b,c 74.7 72.4 72.6 72.3 72.4 76.9 71.1 0 0 28.72 0.6665 28.71 0.6649 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

5a,b,c 74.6 72.5 72.6 72.4 72.4 77.4 71.1 0 0 29.88 0.6931 29.89 0.6921 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

6a,b,c 74.3 72.3 72.4 72.2 72.3 77.7 71.1 0 0 30.96 0.718 30.96 0.7167 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

7a,b,c 74.5 72 72.2 72 72.2 78 71.1 0 0 32.03 0.743 32.08 0.7426 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

8a,b,c 73.7 71.8 72 71.7 72.1 78.3 71.1 0 0 33.2 0.7699 33.23 0.7691 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

9a,b,c 73.2 71.8 71.9 71.7 72 78.6 71.1 0 0 34.41 0.7979 34.39 0.7959 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

10a,b,c 73.6 71.5 71.7 71.4 72 79 71.1 0 0 35.39 0.8205 35.46 0.8206 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

11a,b,c 72.6 71.5 71.7 71.4 71.9 79.4 71.1 0 0 36.56 0.8477 36.61 0.847 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

12a,b,c 73.4 71.4 71.6 71.4 71.9 79.9 71.1 0 0 37.68 0.8732 37.73 0.8728 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

13a,b,c 73.1 71.1 71.3 71.1 71.7 80.2 71.1 0 0 38.92 0.9018 38.89 0.8993 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

14a,b,c 73.4 71.1 71.3 71.1 71.7 80.8 71.1 0 0 39.94 0.9254 39.96 0.924 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

15a,b,c 73.6 71 71.3 71 71.6 81.2 71.1 0 0 41.04 0.9507 41.1 0.95 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

16a,b,c 74.2 71.2 71.4 71.1 71.7 81.9 71.1 0 0 42.35 0.9809 42.34 0.9787 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

17a,b,c 73.6 71.4 71.6 71.3 71.8 82.5 71.1 0 0 43.55 1.0085 43.45 1.0038 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

18a,b,c 74.7 71.6 71.8 71.6 71.9 83.4 71.1 0 0 44.65 1.0337 44.63 1.031 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

19a,b,c 74.5 71.7 71.9 71.7 71.9 84 71.1 0 0 45.86 1.0618 45.85 1.0582 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

20a,b,c 73.8 71.9 72.1 71.8 72.1 84.8 71.1 0 0 47.16 1.0909 47.07 1.0861 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

21a,b,c 74.6 72 72.1 71.9 72.2 85.5 71.1 0 0 48.3 1.1174 48.27 1.1139 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

22a,b,c 74.1 71.9 72.1 71.9 72.2 86.1 71.1 0 0 49.52 1.1455 49.4 1.1399 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

23a,b,c 73.4 71.9 72 71.8 72.2 86.6 71.1 0 0 50.6 1.1702 50.48 1.1645 orange 13.63 13.04 13.32 13.38 9 11.11 0.79 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -30

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-8exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/07/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.9 70.8 71 70.7 71.2 74.4 70.9 0 0 26.56 0.6162 26.54 0.6148 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

2a,b,c 73.9 71 71.1 70.9 71.2 75 70.9 0 0 27.91 0.6477 27.89 0.646 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

3a,b,c 74.2 71.2 71.3 71.1 71.4 75.6 70.9 0 0 29.34 0.6807 29.32 0.6789 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

4a,b,c 73.6 71.3 71.4 71.2 71.4 76.1 70.9 0 0 30.75 0.7134 30.84 0.7141 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

5a,b,c 73.8 71.3 71.4 71.2 71.5 76.7 70.9 0 0 32.35 0.7503 32.25 0.7462 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

6a,b,c 74 71.3 71.4 71.2 71.5 77.2 70.9 0 0 33.73 0.7824 33.72 0.7807 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

7a,b,c 73.8 71.2 71.3 71.1 71.5 77.7 70.9 0 0 35.03 0.8125 35.09 0.8122 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

8a,b,c 72.7 71.1 71.3 71 71.5 78.1 70.9 0 0 36.51 0.8466 36.5 0.8445 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

9a,b,c 72.7 71.1 71.2 71 71.5 78.7 70.9 0 0 38.13 0.884 38.04 0.8801 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

10a,b,c 73.3 71 71.2 70.9 71.4 79.2 70.9 0 0 39.56 0.9169 39.53 0.9143 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

11a,b,c 73 71.1 71.2 71 71.4 79.9 70.9 0 0 41.03 0.9506 41.01 0.948 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

12a,b,c 74.3 71.2 71.3 71.1 71.5 80.6 70.9 0 0 42.65 0.9889 42.66 0.9861 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

13a,b,c 75 71.5 71.6 71.4 71.6 81.4 70.9 0 0 44.04 1.02 44.01 1.0172 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

14a,b,c 74.4 71.7 71.9 71.7 71.8 82.3 70.9 0 0 45.55 1.0544 45.59 1.0532 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

15a,b,c 75.4 71.9 72 71.8 71.9 83 70.9 0 0 47.08 1.0897 47.09 1.0877 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

16a,b,c 74.3 72.1 72.2 72 72.1 84.1 70.9 0 0 48.64 1.1256 48.53 1.12 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

17a,b,c 75.1 72.1 72.2 72 72.1 84.7 70.9 0 0 50.11 1.1591 50.08 1.156 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

18a,b,c 73.9 72 72.2 71.9 72.1 85.6 70.9 0 0 51.55 1.1926 51.61 1.1907 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

19a,b,c 74.9 72 72.1 71.9 72.2 86.2 70.9 0 0 53.26 1.2309 53.09 1.2247 orange 17.17 16.45 16.59 16.85 11.23 13.94 0.99 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -31

11crossover holes-7 exit holes, inline arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 5 degree 11 cross-over holes---7 exit holes

TE slot Arrangement : inline

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 04 / 12 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 72.9 71 71.2 69.8 0.452 0.427 0.429 0.437 0.315 0.386 water 30.13 0.023 70.9 0

10 72.9 71 71.2 69.8 0.699 0.672 0.672 0.684 0.494 0.602 water 30.13 0.028 70.9 0

15 72.9 71 71.2 69.8 1.006 0.942 0.974 0.982 0.692 0.864 water 30.13 0.044 70.9 0

20 72.9 71 71.2 69.8 3.23 3.1 3.19 3.19 2.3 2.82 orange 30.13 0.12 70.9 0

25 72.9 71 71.2 69.8 4.17 4.03 4.09 4.09 2.99 3.61 orange 30.13 0.21 70.9 0

30 72.9 71 71.2 69.8 5.22 5.05 5.09 5.14 3.7 4.56 orange 30.13 0.24 70.9 0

40 72.9 71 71.2 69.8 7.61 7.36 7.43 7.51 5.41 6.6 orange 30.13 0.32 70.9 0

50 72.9 71 71.2 69.8 10.47 10.08 10.37 10.39 7.48 9.14 orange 30.13 0.44 70.9 0

60 72.9 71 71.2 69.8 13.83 13.31 13.56 13.6 9.8 11.99 orange 30.13 0.57 70.9 0

70 72.9 71 71.2 69.8 17.6 16.91 17.19 17.28 12.41 15.18 orange 30.13 0.78 70.9 0

80 72.9 71 71.2 69.8 20.82 20.09 20.35 20.51 14.68 17.92 orange 30.13 0.92 70.9 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross7exit 5blocked

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/12/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.8 71.1 71.2 70.9 71.4 76.5 69.2 0 0 20.16 0.4868 20.24 0.4687 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

2a,b,c 71.8 71.1 71.3 71.0 71.4 78.4 69.2 0 0 21.10 0.4903 21.07 0.4875 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

3a,b,c 71.3 71.1 71.2 71.0 71.4 79.3 69.2 0 0 22.13 0.5140 22.18 0.5131 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

4a,b,c 71.2 71.2 71.3 71.1 71.5 80.4 69.2 0 0 23.04 0.5352 23.13 0.5353 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

5a,b,c 71.7 71.1 71.2 71.0 71.5 81.6 69.2 0 0 24.12 0.5602 24.07 0.5571 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

6a,b,c 71.0 71.2 71.4 71.1 71.6 82.2 69.2 0 0 25.12 0.5833 25.08 0.5802 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

7a,b,c 70.8 71.1 71.3 71.0 71.5 83.1 69.2 0 0 26.13 0.6067 26.10 0.6035 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

8a,b,c 70.8 71.0 71.2 70.9 71.5 84.6 69.2 0 0 27.11 0.6297 27.19 0.6286 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

9a,b,c 70.8 71.0 71.1 70.9 71.5 85.8 69.2 0 0 28.05 0.6512 28.06 0.6489 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

10a,b,c 70.7 71.0 71.2 70.9 71.6 87.1 69.2 0 0 29.10 0.6754 29.13 0.6732 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

11a,b,c 71.0 71.0 71.2 70.7 71.5 87.9 69.2 0 0 30.06 0.6976 29.99 0.6930 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

12a,b,c 70.8 70.9 71.1 70.9 71.5 89.1 69.2 0 0 31.04 0.7202 31.12 0.7184 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

13a,b,c 70.7 71.0 71.2 71.0 71.6 90.6 69.2 0 0 32.04 0.7433 32.02 0.7396 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

14a,b,c 70.5 71.0 71.1 70.9 71.6 92.4 69.2 0 0 33.06 0.7668 33.15 0.7656 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

15a,b,c 71.2 70.9 71.1 70.9 71.5 93.8 69.2 0 0 34.14 0.7921 34.11 0.7877 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

16a,b,c 70.7 70.8 71.0 70.7 71.5 95.3 69.2 0 0 35.06 0.8133 35.21 0.8128 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

17a,b,c 71.1 70.9 71.0 70.8 71.6 96.6 69.2 0 0 36.04 0.8363 36.02 0.8312 water 0.857 0.825 0.828 0.847 0.615 0.745 0.037 30.15

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -32

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross7exit(5 blocked)

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/12/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.1 70.5 70.5 70.4 70.7 75.4 69.2 0 0 21.09 0.4896 21.10 0.4887 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

2a,b,c 72.1 70.6 70.7 70.5 70.8 76.3 69.2 0 0 22.19 0.5152 22.22 0.5143 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

3a,b,c 71.6 70.7 70.7 70.6 70.8 77.0 69.2 0 0 23.32 0.5416 23.31 0.5393 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

4a,b,c 71.5 70.7 70.8 70.5 70.9 78.0 69.2 0 0 24.48 0.5684 24.45 0.5659 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

5a,b,c 72.2 70.8 70.8 70.7 70.9 78.7 69.2 0 0 25.55 0.5931 25.53 0.5908 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

6a,b,c 71.5 70.7 70.8 70.6 70.9 79.7 69.2 0 0 26.63 0.6182 26.64 0.6165 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

7a,b,c 71.9 70.8 70.9 70.7 71.1 80.8 69.2 0 0 27.74 0.6437 27.74 0.6419 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

8a,b,c 71.2 70.9 71.0 70.8 71.1 81.4 69.2 0 0 28.81 0.6688 28.87 0.6677 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

9a,b,c 71.2 70.8 70.9 70.7 71.2 82.9 69.2 0 0 29.89 0.6936 29.96 0.6933 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

10a,b,c 71.1 70.8 71.0 70.7 71.3 83.6 69.2 0 0 31.06 0.7207 31.06 0.7183 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

11a,b,c 71.7 70.9 71.0 70.9 71.2 84.2 69.2 0 0 32.17 0.7464 32.18 0.7440 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

12a,b,c 70.7 70.8 71.0 70.7 71.4 85.9 69.2 0 0 33.23 0.7708 33.20 0.7670 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

13a,b,c 71.5 70.8 70.9 70.8 71.3 87.2 69.2 0 0 34.38 0.7973 34.42 0.7954 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

14a,b,c 70.5 70.8 70.9 70.8 71.3 88.2 69.2 0 0 35.41 0.8212 35.50 0.8201 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

15a,b,c 71.0 70.7 70.8 70.7 71.3 89.9 69.2 0 0 36.53 0.8468 36.57 0.8441 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

16a,b,c 70.7 70.8 70.9 70.7 71.3 90.8 69.2 0 0 37.63 0.8722 37.67 0.8699 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

17a,b,c 70.4 70.6 70.7 70.6 71.2 91.9 69.2 0 0 38.73 0.8973 38.77 0.8950 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

18a,b,c 71.0 70.5 70.7 70.5 71.3 93.5 69.2 0 0 39.80 0.9222 39.80 0.9185 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

19a,b,c 71.3 70.6 70.7 70.5 71.3 94.6 69.2 0 0 40.97 0.9490 40.96 0.9449 orange 4.300 4.160 4.190 4.240 3.050 3.720 0.17 30.13

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/12/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.3 70.6 70.7 70.7 70.7 74.4 69.2 0 0 23.14 0.5375 23.07 0.5342 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

2a,b,c 71.9 70.6 70.7 70.7 70.7 75.2 69.2 0 0 24.22 0.5625 24.31 0.5630 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

3a,b,c 71.7 70.5 70.7 70.7 70.7 76.0 69.2 0 0 25.42 0.5905 25.43 0.5887 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

4a,b,c 71.1 70.5 70.7 70.7 70.7 76.6 69.2 0 0 26.70 0.6200 26.62 0.6163 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

5a,b,c 71.7 70.4 70.7 70.7 70.7 77.2 69.2 0 0 27.89 0.6476 27.86 0.6448 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

6a,b,c 71.6 70.5 70.7 70.7 70.8 78.1 69.2 0 0 29.18 0.6773 29.12 0.6740 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

7a,b,c 71.6 70.4 70.7 70.7 70.8 78.8 69.2 0 0 30.24 0.7019 30.18 0.6983 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

8a,b,c 71.9 70.4 70.7 70.7 70.8 79.5 69.2 0 0 31.43 0.7293 31.45 0.7276 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

9a,b,c 71.4 70.6 70.7 70.7 70.8 80.3 69.2 0 0 32.67 0.7581 32.64 0.7548 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

10a,b,c 72.3 70.6 70.7 70.7 70.8 80.9 69.2 0 0 33.84 0.7850 33.82 0.7822 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

11a,b,c 72.4 70.6 70.7 70.7 71.1 81.8 69.2 0 0 35.03 0.8126 35.07 0.8111 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

12a,b,c 71.8 70.7 70.7 70.7 71.1 82.8 69.2 0 0 36.25 0.8405 36.26 0.8382 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

13a,b,c 71.5 70.8 70.7 70.7 71.1 83.6 69.2 0 0 37.48 0.8689 37.50 0.8666 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

14a,b,c 71.4 70.8 70.7 70.7 71.1 84.5 69.2 0 0 38.73 0.8978 38.69 0.8937 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

15a,b,c 71.7 70.8 70.7 70.7 71.1 85.8 69.2 0 0 39.85 0.9235 39.84 0.9200 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

16a,b,c 71.3 70.8 70.7 70.7 71.3 86.3 69.2 0 0 41.05 0.9510 40.99 0.9465 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

17a,b,c 71.1 70.8 70.7 70.7 71.3 87.3 69.2 0 0 42.26 0.9790 41.94 0.9682 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

18a,b,c 71.9 70.7 70.7 70.7 71.3 88.4 69.2 0 0 43.43 1.0059 43.49 1.0035 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

19a,b,c 71.8 70.7 70.7 70.7 71.3 89.2 69.2 0 0 44.63 1.0334 44.65 1.0299 orange 7.610 7.360 7.430 7.510 5.410 6.600 0.320 30.03

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -33

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:04/12/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.3 71.8 71.9 71.8 72.1 75.5 70.8 0 0 23.82 0.5536 23.78 0.5508 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

2a,b,c 74.8 72.0 72.2 71.9 72.1 76.3 70.8 0 0 25.15 0.5840 25.14 0.5821 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

3a,b,c 74.2 72.1 72.3 72.0 72.3 77.0 70.8 0 0 26.49 0.6149 26.47 0.6129 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

4a,b,c 74.2 72.1 72.3 72.0 72.3 77.6 70.8 0 0 27.75 0.6441 27.80 0.6437 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

5a,b,c 72.9 72.0 72.1 71.9 72.2 78.1 70.8 0 0 29.00 0.6732 29.07 0.6730 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

6a,b,c 72.8 71.9 72.0 71.8 72.2 78.6 70.8 0 0 30.49 0.7074 30.41 0.7038 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

7a,b,c 72.3 71.7 71.9 71.7 72.1 79.1 70.8 0 0 31.69 0.7354 31.61 0.7315 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

8a,b,c 72.0 71.4 71.6 71.3 71.9 79.5 70.8 0 0 32.93 0.7641 32.91 0.7615 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

9a,b,c 72.7 71.2 71.4 71.2 71.8 80.1 70.8 0 0 34.23 0.7938 34.27 0.7929 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

10a,b,c 72.2 71.1 71.3 71.2 71.7 80.7 70.8 0 0 35.56 0.8250 35.57 0.8228 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

11a,b,c 72.1 71.1 71.3 71.1 71.7 81.4 70.8 0 0 36.90 0.8556 36.84 0.8512 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

12a,b,c 73.1 71.2 71.3 71.2 71.7 82.0 70.8 0 0 38.11 0.8833 38.12 0.8813 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

13a,b,c 73.1 71.2 71.4 71.1 71.7 82.9 70.8 0 0 39.44 0.9142 39.33 0.9093 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

14a,b,c 72.8 71.3 71.5 71.2 71.8 83.7 70.8 0 0 40.69 0.9432 40.72 0.9410 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

15a,b,c 73.0 71.3 71.5 71.2 71.8 84.6 70.8 0 0 41.91 0.9712 41.93 0.9693 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

16a,b,c 73.0 71.4 71.6 71.3 71.8 85.2 70.8 0 0 43.27 1.0026 43.16 0.9976 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

17a,b,c 73.2 71.5 71.7 71.5 71.9 86.2 70.8 0 0 44.46 1.0291 44.40 1.0252 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

18a,b,c 73.1 71.5 71.7 71.4 71.9 87.3 70.8 0 0 45.83 1.0617 45.75 1.0559 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

19a,b,c 73.1 71.5 71.6 71.4 71.9 88.1 70.8 0 0 47.15 1.0921 47.21 1.0892 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

20a,b,c 72.4 71.4 71.5 71.3 71.9 89.3 70.8 0 0 48.48 1.1220 48.47 1.1179 orange 11.73 11.31 11.49 11.51 8.29 10.15 0.55 30.01

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/12/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.5 72.2 72.4 72 72.1 75.6 70.7 0 0 24.8 0.5759 24.96 0.578 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

2a,b,c 75.6 72.6 72.7 72.3 72.3 76.3 70.7 0 0 26.23 0.6085 26.24 0.6078 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

3a,b,c 75.1 72.7 72.8 72.5 72.4 76.9 70.7 0 0 27.62 0.6412 27.67 0.6407 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

4a,b,c 75.7 72.8 72.9 72.6 72.6 77.6 70.7 0 0 29.05 0.6743 29.07 0.6731 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

5a,b,c 75.4 72.6 72.8 72.5 72.6 78.1 70.7 0 0 30.48 0.7077 30.47 0.7055 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

6a,b,c 74.8 72.5 72.6 72.4 72.5 78.5 70.7 0 0 31.84 0.739 31.84 0.7369 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

7a,b,c 74 72.4 72.5 72.3 72.4 79 70.7 0 0 33.23 0.7709 33.21 0.7687 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

8a,b,c 73.6 72.2 72.3 72.1 72.4 79.6 70.7 0 0 34.71 0.8051 34.65 0.8013 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

9a,b,c 73.3 72 72.2 71.9 72.3 80.1 70.7 0 0 36.05 0.8361 36.1 0.8352 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

10a,b,c 73.8 71.8 72 71.7 72.2 80.6 70.7 0 0 37.44 0.8684 37.39 0.8646 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

11a,b,c 73.3 71.7 71.8 71.7 72.1 81.2 70.7 0 0 38.81 0.9001 38.82 0.8979 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

12a,b,c 73 71.6 71.8 71.6 72.1 81.8 70.7 0 0 40.23 0.9326 40.14 0.928 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

13a,b,c 72.6 71.5 71.7 71.5 72 82.4 70.7 0 0 41.6 0.9642 41.65 0.9625 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

14a,b,c 72.8 71.4 71.6 71.4 71.9 83.1 70.7 0 0 43.04 0.9975 43.09 0.9955 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

15a,b,c 73.1 71.3 71.5 71.3 71.9 83.9 70.7 0 0 44.47 1.0303 44.44 1.0259 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

16a,b,c 72.7 71.3 71.4 71.3 71.9 84.5 70.7 0 0 45.89 1.0629 45.89 1.0596 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

17a,b,c 72.1 71.2 71.4 71.2 71.9 85.3 70.7 0 0 47.25 1.0943 47.2 1.0894 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

18a,b,c 72.3 71.1 71.3 71.1 71.8 86 70.7 0 0 48.61 1.1253 48.59 1.1214 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

19a,b,c 72.9 71.3 71.4 71.2 71.9 86.8 70.7 0 0 50.05 1.1587 50 1.1537 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

20a,b,c 73.3 71.3 71.4 71.2 71.9 87.8 70.7 0 0 51.52 1.1922 51.49 1.1873 orange 16.95 16.29 16.57 16.64 11.99 14.65 0.72 29.98

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -34

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-7exit

inline

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:04/12/2012

80 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.5 72.2 72.3 72.1 72.2 75.4 70 0 0 25.49 0.5919 25.69 0.5945 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

2a,b,c 74.8 72.1 72.3 72 72.3 76 70 0 0 27.07 0.6287 27.05 0.6265 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

3a,b,c 74.8 72.2 72.3 72 72.2 76.4 70 0 0 28.57 0.6632 28.6 0.6623 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

4a,b,c 74.4 72 72.2 71.9 72.2 77 70 0 0 30.11 0.699 29.99 0.6943 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

5a,b,c 73.7 71.7 72.1 71.9 72.2 77.4 70 0 0 31.55 0.7324 31.56 0.7303 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

6a,b,c 73.1 71.8 71.9 71.6 72.1 77.9 70 0 0 33.07 0.7676 33 0.7638 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

7a,b,c 74 71.7 71.9 71.7 72 78.4 70 0 0 34.61 0.8031 34.51 0.7984 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

8a,b,c 73.1 71.4 71.8 71.6 72 78.9 70 0 0 36 0.8353 36.05 0.8342 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

9a,b,c 72.8 71.3 71.7 71.3 72 79.5 70 0 0 37.59 0.8719 37.6 0.8697 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

10a,b,c 72.8 71.3 71.5 71.2 71.9 80 70 0 0 39.12 0.9072 38.93 0.9004 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

11a,b,c 72.8 71.3 71.5 71.2 71.8 80.7 70 0 0 40.43 0.9375 40.36 0.9334 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

12a,b,c 72.9 71.3 71.5 71.3 71.8 81.2 70 0 0 42.06 0.975 41.99 0.9706 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

13a,b,c 72.9 71.4 71.5 71.3 71.8 82 70 0 0 43.57 1.0096 43.58 1.0077 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

14a,b,c 73.5 71.4 71.6 71.2 71.8 82.6 70 0 0 45.06 1.0438 45.08 1.0413 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

15a,b,c 73.6 71.5 71.5 71.3 71.8 83.5 70 0 0 46.52 1.0771 46.53 1.0746 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

16a,b,c 72.8 71.5 71.6 71.3 71.9 84.4 70 0 0 48.1 1.1139 48.03 1.1096 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

17a,b,c 73.7 71.5 71.6 71.4 71.9 85.1 70 0 0 49.51 1.1462 49.54 1.1433 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

18a,b,c 73.7 71.3 71.5 71.2 71.8 86.4 70 0 0 50.96 1.18 50.94 1.1761 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

19a,b,c 73 71.4 71.6 71.3 71.9 87.3 70 0 0 52.63 1.2184 52.54 1.2119 orange 20.82 20.09 20.35 20.51 14.68 17.92 0.92 29.99

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -35

11crossover holes-12 exit holes, staggered arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---9 exit holes

TE slot Arrangement : staggered

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 05 / 08 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 70.3 70.6 70.8 71.5 0.316 0.3 0.302 0.307 0.188 0.251 water 29.95 0.019 70.5 0

10 70.3 70.6 70.8 71.5 0.519 0.493 0.499 0.504 0.312 0.415 water 29.95 0.038 70.5 0

15 70.3 70.6 70.8 71.5 0.772 0.736 0.738 0.753 0.485 0.626 water 29.95 0.058 70.5 0

20 70.3 70.6 70.8 71.5 2.62 2.42 2.51 2.58 1.66 2.17 orange 29.95 0.22 70.5 0

25 70.3 70.6 70.8 71.5 3.61 3.39 3.45 3.51 2.29 2.99 orange 29.95 0.28 70.5 0

30 70.3 70.6 70.8 71.5 4.2 4.01 4.09 4.17 2.72 3.5 orange 29.95 0.28 70.5 0

40 70.3 70.6 70.8 71.5 6.26 5.91 6.01 6.11 3.99 5.19 orange 29.95 0.41 70.5 0

50 70.3 70.6 70.8 71.5 8.69 8.34 8.49 8.51 5.61 7.65 orange 29.95 0.6 70.5 0

60 70.3 70.6 70.8 71.5 11.5 11.01 11.15 11.16 7.49 9.59 orange 29.95 0.79 70.5 0

70 70.3 70.6 70.8 71.5 14.28 13.62 13.82 13.98 9.26 11.81 orange 29.95 0.94 70.5 0

80 70.3 70.6 70.8 71.5 17.62 16.96 17.32 17.28 11.5 14.78 orange 29.95 1.26 70.5 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 68.7 70.8 71.0 70.9 72.1 81.9 72.6 0 0 20.75 0.4819 20.71 0.4797 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

2a,b,c 68.7 70.8 71.0 70.9 72.1 85.2 72.6 0 0 21.56 0.5004 21.52 0.4979 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

3a,b,c 68.7 70.8 71.0 70.8 72.1 87.6 72.6 0 0 22.13 0.5137 22.25 0.5148 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

4a,b,c 68.7 70.8 71.0 70.8 72.1 89.8 72.6 0 0 22.98 0.5334 23.02 0.5328 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

5a,b,c 68.7 70.8 71.0 70.8 72.0 91.5 72.6 0 0 23.64 0.5488 23.78 0.5499 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

6a,b,c 68.7 70.8 71.0 70.7 72.0 93.1 72.6 0 0 24.47 0.5679 24.46 0.5659 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

7a,b,c 68.7 70.8 71.0 70.7 72.0 95.1 72.6 0 0 25.01 0.5804 25.04 0.5790 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

8a,b,c 68.7 70.8 71.0 70.7 72.0 96.6 72.6 0 0 25.77 0.5981 25.77 0.5957 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

9a,b,c 68.7 70.8 71.0 70.7 72.0 98.2 72.6 0 0 26.30 0.6102 26.37 0.6096 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

10a,b,c 68.7 70.8 71.0 70.7 72.0 99.8 72.6 0 0 27.08 0.6284 27.06 0.6254 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

11a,b,c 68.7 70.4 71.9 70.6 72.0 101.9 72.6 0 0 27.74 0.6437 27.75 0.6412 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

12a,b,c 68.7 70.4 71.9 70.6 72.0 103.2 72.6 0 0 28.41 0.6591 28.48 0.6580 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

13a,b,c 68.7 70.4 71.9 70.6 72.0 104.7 72.6 0 0 29.09 0.6747 29.11 0.6727 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

14a,b,c 68.7 70.4 71.9 70.4 71.9 107.1 72.6 0 0 29.81 0.6911 29.86 0.6897 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

15a,b,c 68.7 70.4 71.9 70.4 71.9 108.8 72.6 0 0 30.39 0.7046 30.51 0.7041 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

16a,b,c 68.7 70.4 71.9 70.4 71.9 111.0 72.6 0 0 31.18 0.7230 31.28 0.7220 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

17a,b,c 68.7 70.4 71.9 70.4 71.9 113.1 72.6 0 0 32.25 0.7475 32.32 0.7459 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

18a,b,c 68.7 70.4 71.9 70.4 71.9 115.6 72.6 0 0 33.18 0.7689 33.22 0.7664 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

19a,b,c 68.7 70.4 71.9 70.4 71.9 117.9 72.6 0 0 34.18 0.7921 34.10 0.7869 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

20a,b,c 68.7 70.4 71.9 70.5 71.9 121.0 72.6 0 0 35.20 0.8160 35.00 0.8072 water 0.453 0.424 0.433 0.438 0.246 0.246 0.036 29.8

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -36

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.8 71.0 71.2 70.9 71.7 82.6 72.6 0 0 22.51 0.5226 22.35 0.5173 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

2a,b,c 71.8 71.1 71.3 71.0 71.7 85.1 72.6 0 0 23.23 0.5394 23.35 0.5405 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

3a,b,c 71.8 71.2 71.3 71.1 71.8 87.2 72.6 0 0 24.21 0.5621 24.26 0.5613 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

4a,b,c 71.8 71.2 71.4 71.2 71.9 88.9 72.6 0 0 25.09 0.5826 25.13 0.5818 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

5a,b,c 71.8 71.3 71.5 71.3 71.9 90.6 72.6 0 0 26.25 0.6093 26.17 0.6054 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

6a,b,c 71.8 71.4 71.6 71.3 72.0 92.4 72.6 0 0 27.11 0.6291 27.20 0.6292 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

7a,b,c 71.8 71.4 71.6 71.3 72.2 94.3 72.6 0 0 28.52 0.6555 28.34 0.6554 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

8a,b,c 71.8 71.4 71.6 71.3 72.2 97.0 72.6 0 0 29.12 0.6758 29.29 0.6772 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

9a,b,c 71.8 71.4 71.6 71.3 72.2 98.8 72.6 0 0 30.21 0.7009 30.34 0.7015 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

10a,b,c 71.8 71.4 71.5 71.3 72.2 100.6 72.6 0 0 31.23 0.7243 31.26 0.7224 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

11a,b,c 71.0 71.4 71.5 71.3 72.2 102.9 72.6 0 0 32.24 0.7476 32.33 0.7471 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

12a,b,c 71.0 71.4 71.6 71.3 72.2 104.9 72.6 0 0 33.26 0.7713 33.41 0.7717 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

13a,b,c 71.0 71.4 71.6 71.3 72.2 107.3 72.6 0 0 33.97 0.7877 34.09 0.7873 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

14a,b,c 71.0 71.4 71.6 71.3 72.2 109.3 72.6 0 0 34.68 0.8040 34.61 0.7991 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

15a,b,c 71.0 71.4 71.6 71.3 72.2 111.4 72.6 0 0 35.15 0.8148 35.10 0.8104 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

16a,b,c 71.0 71.4 71.5 71.3 72.2 112.6 72.6 0 0 35.64 0.8262 35.64 0.8228 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

17a,b,c 71.0 71.4 71.5 71.3 72.2 113.9 72.6 0 0 36.36 0.8427 36.26 0.8368 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

18a,b,c 71.0 71.4 71.5 71.3 72.2 116.1 72.6 0 0 37.12 0.8604 37.18 0.8581 water 1.012 0.943 0.964 0.969 0.556 0.556 0.087 29.81

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.0 72.1 72.3 72.1 72.6 82.5 72.6 0 0 23.28 0.5407 23.17 0.5364 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

2a,b,c 73.2 72.1 72.3 72.1 72.6 84.1 72.6 0 0 24.10 0.5595 24.02 0.5560 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

3a,b,c 72.7 72.1 72.3 72.0 72.6 85.6 72.6 0 0 25.02 0.5808 25.06 0.5800 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

4a,b,c 72.8 72.1 72.3 71.9 72.6 87.2 72.6 0 0 26.11 0.6061 26.21 0.6065 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

5a,b,c 72.5 72.1 72.3 72.0 72.6 88.8 72.6 0 0 27.12 0.6296 27.13 0.6277 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

6a,b,c 73.0 72.1 72.2 72.0 72.6 90.2 72.6 0 0 28.14 0.6532 28.00 0.6480 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

7a,b,c 72.7 72.1 72.2 72.1 72.6 91.4 72.6 0 0 29.17 0.6771 29.05 0.6725 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

8a,b,c 73.1 72.1 72.2 72.0 72.6 93.4 72.6 0 0 30.11 0.6986 30.19 0.6981 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

9a,b,c 72.6 72.1 72.2 72.0 72.6 94.7 72.6 0 0 31.14 0.7225 31.14 0.7201 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

10a,b,c 73.1 72.1 72.2 72.0 72.6 96.6 72.6 0 0 32.13 0.7454 32.15 0.7434 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

11a,b,c 72.4 72.0 72.2 72.0 72.6 98.1 72.6 0 0 33.19 0.7699 33.20 0.7674 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

12a,b,c 72.9 72.0 72.0 72.0 72.6 100.1 72.6 0 0 34.01 0.7890 34.11 0.7884 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

13a,b,c 73.0 72.0 72.0 71.9 72.6 102.1 72.6 0 0 35.19 0.8161 35.22 0.8139 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

14a,b,c 72.3 72.0 72.0 71.8 72.6 104.0 72.6 0 0 36.21 0.8397 36.41 0.8412 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

15a,b,c 72.3 72.0 72.0 71.8 72.6 105.8 72.6 0 0 37.39 0.8666 37.52 0.8664 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

16a,b,c 72.9 72.0 72.0 71.8 72.6 107.8 72.6 0 0 38.09 0.8828 38.19 0.8821 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

17a,b,c 72.5 72.0 72.0 71.8 72.6 109.9 72.6 0 0 39.07 0.9054 39.12 0.9030 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

18a,b,c 72.7 72.0 72.0 71.8 72.6 111.7 72.6 0 0 40.04 0.9272 40.11 0.9259 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

19a,b,c 72.7 72.0 72.0 71.7 72.6 114.2 72.6 0 0 41.13 0.9527 41.12 0.9490 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

20a,b,c 72.9 72.0 72.0 71.7 72.6 115.8 72.6 0 0 42.02 0.9731 42.00 0.9690 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

21a,b,c 72.9 72.0 72.0 71.7 72.6 118.9 72.6 0 0 43.17 0.9996 43.11 0.9942 orange 4.31 4.01 4.19 4.19 2.49 2.49 0.38 29.83

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -37

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.4 72.5 72.6 72.4 72.9 82.5 72.3 0 0 24.76 0.5750 24.69 0.5717 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

2a,b,c 74.4 72.5 72.6 72.4 72.9 83.8 72.3 0 0 25.49 0.5917 25.58 0.5925 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

3a,b,c 74.4 72.5 72.6 72.4 72.9 85.0 72.3 0 0 26.54 0.6163 26.56 0.6153 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

4a,b,c 74.4 72.5 72.6 72.4 72.9 86.1 72.3 0 0 27.58 0.6402 27.66 0.6402 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

5a,b,c 74.4 72.5 72.6 72.4 72.9 87.3 72.3 0 0 28.73 0.6668 28.63 0.6624 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

6a,b,c 74.4 72.5 72.6 72.4 72.9 88.6 72.3 0 0 29.61 0.6873 29.69 0.6869 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

7a,b,c 74.4 72.5 72.6 72.4 73.1 90.0 72.3 0 0 30.61 0.7104 30.53 0.7064 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

8a,b,c 74.4 72.5 72.6 72.6 73.1 91.3 72.3 0 0 31.65 0.7343 31.64 0.7320 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

9a,b,c 74.4 72.5 72.6 72.6 73.1 92.8 72.3 0 0 32.60 0.7562 32.57 0.7531 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

10a,b,c 74.4 72.5 72.6 72.6 73.1 94.0 72.3 0 0 33.52 0.7776 33.50 0.7747 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

11a,b,c 73.8 72.7 72.6 72.6 73.1 95.6 72.3 0 0 34.51 0.8005 34.59 0.7998 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

12a,b,c 73.8 72.7 72.6 72.6 73.1 96.6 72.3 0 0 35.54 0.8243 35.58 0.8223 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

13a,b,c 74.2 72.7 72.6 72.6 73.1 98.2 72.3 0 0 36.63 0.8495 36.46 0.8426 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

14a,b,c 73.6 72.7 72.6 72.6 73.1 100.0 72.3 0 0 37.52 0.8700 37.62 0.8696 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

15a,b,c 73.9 72.7 72.6 72.4 73.1 101.9 72.3 0 0 38.65 0.8959 38.61 0.8918 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

16a,b,c 73.6 72.7 72.6 72.4 73.1 103.4 72.3 0 0 39.52 0.9162 39.51 0.9126 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

17a,b,c 74.4 72.4 72.6 72.4 73.1 104.8 72.3 0 0 40.48 0.9380 40.65 0.9385 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

18a,b,c 74.4 72.4 72.6 72.4 73.1 106.2 72.3 0 0 41.58 0.9635 41.55 0.9593 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

19a,b,c 74.4 72.4 72.6 72.4 73.1 108.4 72.3 0 0 42.57 0.9861 42.73 0.9864 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

20a,b,c 74.4 72.4 72.6 72.4 73.1 109.9 72.3 0 0 43.53 1.0083 43.46 1.0029 orange 6.7 6.28 6.41 6.49 3.88 3.89 0.52 29.86

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

69psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.2 73.4 73.5 73.3 73.4 81.4 72.2 0 0 26.04 0.6045 26.12 0.6045 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

2a,b,c 75.9 73.4 73.5 73.4 73.5 83.2 72.2 0 0 27.01 0.6273 27.14 0.6284 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

3a,b,c 76.0 73.4 73.5 73.4 73.5 84.2 72.2 0 0 28.14 0.6534 28.17 0.8524 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

4a,b,c 76.3 73.4 73.5 73.3 73.6 85.5 72.2 0 0 29.28 0.6797 29.22 0.6763 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

5a,b,c 76.3 73.4 73.5 73.3 73.6 86.4 72.2 0 0 30.21 0.7013 30.04 0.6954 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

6a,b,c 76.2 73.4 73.5 73.3 73.6 87.6 72.2 0 0 31.10 0.7218 31.01 0.7174 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

7a,b,c 76.2 73.4 73.5 73.4 73.6 88.6 72.2 0 0 32.03 0.7434 32.09 0.7452 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

8a,b,c 75.2 73.4 73.5 73.4 73.6 89.7 72.2 0 0 33.15 0.7692 33.19 0.7675 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

9a,b,c 75.3 73.4 73.4 73.3 73.6 90.8 72.2 0 0 34.07 0.7905 34.15 0.7898 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

10a,b,c 75.2 73.4 73.4 73.2 73.6 92.0 72.2 0 0 35.12 0.8148 35.04 0.8104 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

11a,b,c 75.7 73.1 73.4 73.2 73.6 93.1 72.2 0 0 36.16 0.8387 36.15 0.8358 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

12a,b,c 75.7 73.1 73.2 73.2 73.5 94.3 72.2 0 0 37.17 0.8620 37.33 0.8629 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

13a,b,c 75.9 73.2 73.2 73.2 73.5 95.5 72.2 0 0 38.15 0.8846 38.19 0.8828 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

14a,b,c 75.4 73.2 73.2 73.1 73.5 96.8 72.2 0 0 39.15 0.9077 39.24 0.9068 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

15a,b,c 75.1 73.2 73.2 73.1 73.6 98.0 72.2 0 0 40.24 0.9328 40.09 0.9265 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

16a,b,c 75.2 73.1 73.2 73.1 73.5 99.1 72.2 0 0 41.04 0.9512 41.09 0.9494 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

17a,b,c 75.2 73.1 73.2 73.1 73.5 100.7 72.2 0 0 42.12 0.9761 42.03 0.9713 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

18a,b,c 75.6 73.1 73.2 73.0 73.5 102.0 72.2 0 0 43.13 0.9993 43.10 0.9953 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

19a,b,c 75.1 73.1 73.1 73.1 73.5 103.5 72.2 0 0 44.03 1.0199 44.13 1.0190 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

20a,b,c 74.8 73.1 73.1 72.8 73.5 105.1 72.2 0 0 45.13 1.0454 45.18 1.0429 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

21a,b,c 75.1 73.1 73.1 72.8 73.4 106.8 72.2 0 0 46.21 1.0701 46.08 1.0631 orange 9.82 9.25 9.48 9.52 5.69 5.73 0.86 29.88

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -38

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ all open

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.0 66.1 66.5 66.1 67.7 82.1 72.1 0 0 32.23 0.7485 32.29 0.7474 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

2a,b,c 72.7 66.4 66.8 66.4 67.8 82.8 72.1 0 0 33.13 0.7687 33.07 0.7655 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

3a,b,c 73.1 67.5 67.7 67.3 68.3 84.1 72.1 0 0 34.05 0.7904 33.99 0.7865 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

4a,b,c 73.3 68.1 68.3 68.0 68.8 85.4 72.1 0 0 35.15 0.8158 35.13 0.8127 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

5a,b,c 73.8 68.5 68.7 68.4 69.1 86.6 72.1 0 0 36.09 0.8375 36.13 0.8359 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

6a,b,c 73.7 68.9 69.1 68.8 69.4 87.7 72.1 0 0 37.04 0.8595 37.05 0.8570 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

7a,b,c 73.8 69.3 69.5 69.2 69.7 88.9 72.1 0 0 38.11 0.8839 38.15 0.8822 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

8a,b,c 74.4 69.7 69.8 69.5 70.0 90.2 72.1 0 0 39.00 0.9044 38.90 0.8994 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

9a,b,c 73.9 69.9 70.0 69.8 70.2 91.4 72.1 0 0 40.07 0.9293 40.02 0.9252 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

10a,b,c 74.0 70.1 70.2 69.9 70.5 92.7 72.1 0 0 41.06 0.9519 41.01 0.9478 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

11a,b,c 74.4 70.4 70.4 70.2 70.7 94.2 72.1 0 0 42.18 0.9779 42.12 0.9478 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

12a,b,c 74.4 70.6 70.6 70.4 70.9 95.4 72.1 0 0 43.03 0.9972 43.00 0.9934 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

13a,b,c 74.6 70.8 70.8 70.6 71.3 97.2 72.1 0 0 44.07 1.0212 44.15 1.0196 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

14a,b,c 75.3 71.1 71.1 71.0 71.6 98.6 72.1 0 0 44.95 1.0420 44.91 1.0373 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

15a,b,c 74.7 71.4 71.3 71.3 71.7 100.4 72.1 0 0 46.05 1.0667 46.15 1.0653 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

16a,b,c 74.7 71.5 71.6 71.4 71.9 101.4 72.1 0 0 46.89 1.0681 46.90 1.0823 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

17a,b,c 74.9 71.6 71.7 71.4 71.9 102.5 72.1 0 0 47.70 1.1044 47.70 1.1007 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

18a,b,c 75.5 71.6 71.9 71.5 72.1 104.2 72.1 0 0 48.82 1.1307 48.92 1.1287 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

19a,b,c 75.5 71.7 71.9 71.6 72.1 105.8 72.1 0 0 49.96 1.1563 50.02 1.1536 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

20a,b,c 75.6 71.9 72.1 71.8 72.2 107.7 72.1 0 0 51.26 1.1863 51.37 1.1845 orange 12.31 11.44 11.81 11.91 7.01 7.14 1.11 29.89

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -39

11crossover holes-10 exit holes, staggered arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---8 exit holes

TE slot Arrangement : staggered

Experimentalist : Xiao Huang Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 05 / 07 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 70.9 71.1 71.2 71.4 0.41 0.397 0.397 0.402 0.265 0.357 water 30.11 0.024 71.1 0

10 70.9 71.1 71.2 71.4 0.718 0.646 0.673 0.665 0.439 0.582 water 30.11 0.041 71.1 0

15 70.9 71.1 71.2 71.4 2.42 2.32 2.35 2.38 0.646 0.832 water 30.11 0.058 71.1 0

20 70.9 71.1 71.2 71.4 3.29 3.17 3.2 3.19 2.23 2.85 water/orange 30.11 0.2 71.1 0

25 70.9 71.1 71.2 71.4 4.7 4.49 4.58 4.61 3.23 4.11 orange 30.11 0.28 71.1 0

30 70.9 71.1 71.2 71.4 5.25 5.09 5.09 5.19 3.61 4.58 orange 30.11 0.35 71.1 0

40 70.9 71.1 71.2 71.4 7.89 7.59 7.59 7.69 5.37 6.88 orange 30.11 0.43 71.1 0

50 70.9 71.1 71.2 71.4 10.62 10.19 10.41 10.5 7.32 9.39 orange 30.11 0.62 71.1 0

60 70.9 71.1 71.2 71.4 14.01 13.52 13.69 13.71 9.61 12.31 orange 30.11 0.88 71.1 0

70 70.9 71.1 71.2 71.4 17.2 16.59 16.77 16.91 11.79 15.06 orange 30.11 1 71.1 0

80 70.9 71.1 71.2 71.4 21.55 20.79 21.05 21.09 14.79 18.94 orange 30.11 1.22 71.1 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover10exits 2blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.5 70.5 70.7 70.5 71.7 77.2 72.2 0 0 20.07 0.4662 20.01 0.4634 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

2a,b,c 69.4 70.5 70.7 70.5 71.7 78.9 72.2 0 0 20.83 0.4836 20.84 0.4825 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

3a,b,c 68.8 70.5 70.7 70.5 71.7 80.4 72.2 0 0 21.47 0.4985 21.53 0.4986 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

4a,b,c 69.1 70.4 70.7 70.5 71.7 81.0 72.2 0 0 22.21 0.5157 22.26 0.5151 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

5a,b,c 68.8 70.4 70.6 70.4 71.7 82.3 72.2 0 0 23.07 0.5356 23.12 0.5349 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

6a,b,c 68.6 70.4 70.6 70.4 71.7 83.1 72.2 0 0 23.89 0.5546 23.89 0.5529 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

7a,b,c 69.3 70.4 70.6 70.4 71.7 84.0 72.2 0 0 24.72 0.5738 24.72 0.5720 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

8a,b,c 69.1 70.3 70.6 70.4 71.7 84.9 72.2 0 0 25.46 0.5909 25.56 0.5913 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

9a,b,c 69.2 70.3 70.5 70.3 71.7 85.8 72.2 0 0 26.47 0.6144 26.47 0.6122 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

10a,b,c 68.5 70.2 70.4 70.2 71.7 86.8 72.2 0 0 27.26 0.6327 27.39 0.6333 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

11a,b,c 68.3 70.1 70.3 70.1 71.6 88.0 72.2 0 0 28.19 0.6541 28.34 0.6554 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

12a,b,c 68.6 70.1 70.3 70.1 71.6 89.1 72.2 0 0 29.19 0.6771 29.30 0.6775 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

13a,b,c 68.7 70.1 70.4 70.2 71.7 90.4 72.2 0 0 30.25 0.7017 30.13 0.6966 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

14a,b,c 68.7 70.2 70.5 70.2 71.7 91.6 72.2 0 0 31.18 0.7233 31.18 0.7207 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

15a,b,c 68.7 70.2 70.4 70.3 71.8 93.2 72.2 0 0 32.13 0.7450 32.15 0.7430 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

16a,b,c 68.7 70.2 70.4 70.3 71.8 94.1 72.2 0 0 33.03 0.7659 33.08 0.7643 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

17a,b,c 68.5 70.2 70.4 70.2 71.8 96.3 72.2 0 0 33.90 0.7859 33.92 0.7835 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

18a,b,c 68.9 70.2 70.4 70.2 71.8 97.0 72.2 0 0 34.95 0.8100 34.80 0.8035 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

19a,b,c 68.5 70.2 70.4 70.2 71.8 99.0 72.2 0 0 35.70 0.8273 35.55 0.8206 water 0.582 0.551 0.562 0.566 0.359 0.439 0.03 29.91

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -40

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover10exit 2 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.0 71.1 71.3 71.1 71.9 76.5 72.3 0 0 21.13 0.4909 21.15 0.4899 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

2a,b,c 70.8 70.9 71.1 70.9 71.8 77.5 72.3 0 0 22.00 0.5109 22.05 0.5105 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

3a,b,c 70.4 70.9 71.0 70.8 71.8 78.2 72.3 0 0 22.93 0.5325 22.93 0.5308 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

4a,b,c 70.8 70.8 71.0 70.8 71.8 78.7 72.3 0 0 23.85 0.5539 23.80 0.5510 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

5a,b,c 70.7 70.8 71.0 70.7 71.8 79.5 72.3 0 0 24.69 0.5732 24.70 0.5716 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

6a,b,c 70.4 70.8 71.0 70.7 71.8 80.3 72.3 0 0 25.58 0.5939 25.70 0.5949 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

7a,b,c 70.2 70.7 71.0 70.7 71.8 81.1 72.3 0 0 26.56 0.6164 26.62 0.6160 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

8a,b,c 70.9 70.9 71.1 70.8 71.8 82.0 72.3 0 0 27.55 0.6395 27.64 0.6396 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

9a,b,c 70.4 70.9 71.1 70.9 71.8 82.6 72.3 0 0 28.58 0.6635 28.63 0.6624 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

10a,b,c 70.3 70.9 71.1 70.8 71.9 83.7 72.3 0 0 29.60 0.6870 29.61 0.6847 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

11a,b,c 70.4 70.9 71.1 70.8 71.9 84.4 72.3 0 0 30.47 0.7070 30.53 0.7063 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

12a,b,c 70.5 70.8 71.0 70.8 71.9 85.3 72.3 0 0 31.46 0.7299 31.58 0.7303 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

13a,b,c 70.2 70.8 71.0 70.8 71.8 86.2 72.3 0 0 32.51 0.7543 32.56 0.7528 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

14a,b,c 70.1 70.6 70.8 70.6 71.8 87.2 72.3 0 0 33.56 0.7785 33.62 0.7769 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

15a,b,c 69.9 70.5 70.8 70.5 71.8 88.3 72.3 0 0 34.48 0.7999 34.72 0.8025 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

16a,b,c 70.3 70.5 70.8 70.5 71.8 89.2 72.3 0 0 35.58 0.8250 35.51 0.8207 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

17a,b,c 70.5 70.5 70.7 70.6 71.8 90.3 72.3 0 0 36.52 0.8466 36.56 0.8448 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

18a,b,c 69.8 70.5 70.7 70.5 71.8 91.5 72.3 0 0 37.59 0.8713 37.51 0.8665 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

19a,b,c 70.6 70.5 70.7 70.5 71.8 92.1 72.3 0 0 38.51 0.8923 38.57 0.8908 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

20a,b,c 69.8 70.5 70.7 70.5 71.8 93.6 72.3 0 0 39.64 0.9185 39.69 0.9164 orange 3.010 2.810 2.850 2.910 1.820 2.290 0.100 29.91

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 10exit 2 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.4 71.2 71.4 71.1 71.9 76.9 71.6 0 0 21.99 0.5109 21.95 0.5084 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

2a,b,c 71.8 71.2 71.3 71.1 71.9 77.2 71.6 0 0 22.93 0.5326 22.98 0.5322 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

3a,b,c 71.6 71.1 71.3 71.1 71.9 77.7 71.6 0 0 24.04 0.5583 24.09 0.5580 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

4a,b,c 71.3 71.1 71.3 71.1 71.9 78.5 71.6 0 0 24.90 0.5783 25.04 0.5797 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

5a,b,c 71.7 71.1 71.3 71.0 71.9 79.0 71.6 0 0 25.97 0.6031 26.00 0.6019 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

6a,b,c 71.4 71.0 71.2 71.0 71.9 79.4 71.6 0 0 27.02 0.6274 27.02 0.6256 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

7a,b,c 71.7 71.0 71.2 71.0 71.8 80.1 71.6 0 0 27.97 0.6498 28.05 0.6492 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

8a,b,c 71.3 71.0 71.2 71.0 71.8 80.8 71.6 0 0 29.03 0.6737 29.03 0.6719 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

9a,b,c 71.5 71.0 71.2 71.0 71.8 81.3 71.6 0 0 30.19 0.7007 30.15 0.6978 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

10a,b,c 71.3 71.0 71.2 70.9 71.8 82.1 71.6 0 0 31.37 0.7279 31.29 0.7242 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

11a,b,c 71.5 70.9 71.1 70.9 71.8 82.7 71.6 0 0 32.41 0.7521 32.41 0.7497 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

12a,b,c 71.1 70.9 71.1 70.9 71.8 83.6 71.6 0 0 33.80 0.7841 33.71 0.7804 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

13a,b,c 71.2 70.8 71.0 70.8 71.8 84.4 71.6 0 0 34.83 0.8081 34.93 0.8074 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

14a,b,c 71.2 70.7 70.9 70.7 71.8 85.3 71.6 0 0 35.99 0.8348 36.09 0.8345 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

15a,b,c 71.0 70.7 71.0 70.7 71.8 86.4 71.6 0 0 37.31 0.8654 37.39 0.8645 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

16a,b,c 71.5 70.7 70.9 70.7 71.8 87.4 71.6 0 0 38.69 0.8970 38.64 0.8930 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

17a,b,c 70.8 70.7 71.0 70.7 71.8 88.6 71.6 0 0 39.94 0.9259 40.00 0.9248 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

18a,b,c 71.1 70.8 71.0 70.7 71.9 89.7 71.6 0 0 41.38 0.9590 41.29 0.9537 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

19a,b,c 70.2 70.7 70.9 70.6 71.9 90.5 71.6 0 0 42.49 0.9844 42.54 0.9824 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

20a,b,c 70.6 70.6 70.8 70.6 71.8 91.6 71.6 0 0 43.56 1.0087 43.34 1.0004 orange 5.460 5.100 5.210 5.310 3.390 4.170 0.330 29.9

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -41

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11corssover-10exit 2blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.4 72.6 72.7 72.5 72.9 76.9 71.4 0 0 22.64 0.5258 22.59 0.5232 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

2a,b,c 74.5 72.8 72.9 72.7 73.1 77.6 71.4 0 0 23.63 0.5489 23.54 0.5448 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

3a,b,c 74.9 72.8 72.9 72.7 73.2 78.0 71.4 0 0 24.55 0.5701 24.61 0.5698 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

4a,b,c 74.5 72.8 72.9 72.7 73.2 78.5 71.4 0 0 25.57 0.5937 25.59 0.5927 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

5a,b,c 74.2 72.9 73.0 72.8 73.3 79.0 71.4 0 0 26.56 0.6167 26.58 0.6153 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

6a,b,c 74.2 72.9 73.0 72.8 73.3 79.5 71.4 0 0 27.59 0.6405 27.51 0.6370 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

7a,b,c 74.9 73.0 73.1 72.9 73.4 80.1 71.4 0 0 28.63 0.6645 28.65 0.6631 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

8a,b,c 74.0 72.8 72.9 72.7 73.4 80.7 71.4 0 0 29.53 0.6854 29.58 0.6843 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

9a,b,c 73.9 72.7 72.9 72.6 73.3 81.2 71.4 0 0 30.66 0.7116 30.59 0.7079 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

10a,b,c 73.9 72.6 72.7 72.5 73.2 81.6 71.4 0 0 31.56 0.7325 31.68 0.7331 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

11a,b,c 73.9 72.4 72.6 72.4 73.0 82.3 71.4 0 0 32.52 0.7547 32.59 0.7544 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

12a,b,c 73.0 71.9 72.1 71.8 72.8 82.7 71.4 0 0 33.65 0.7807 33.57 0.7772 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

13a,b,c 72.1 71.5 71.8 71.5 72.6 83.0 71.4 0 0 34.56 0.8017 34.56 0.7995 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

14a,b,c 72.5 71.4 71.7 71.3 72.5 83.4 71.4 0 0 35.64 0.8267 35.71 0.8259 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

15a,b,c 71.9 71.3 71.6 71.3 72.4 84.1 71.4 0 0 36.89 0.8556 36.95 0.8544 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

16a,b,c 71.4 71.1 71.4 71.0 72.3 84.8 71.4 0 0 38.07 0.8832 38.04 0.8795 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

17a,b,c 72.3 71.2 71.5 71.2 72.4 85.5 71.4 0 0 39.34 0.9119 39.31 0.9085 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

18a,b,c 72.3 71.2 71.5 71.2 72.4 86.2 71.4 0 0 40.80 0.9458 40.77 0.9421 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

19a,b,c 72.5 71.3 71.5 71.2 72.4 87.5 71.4 0 0 41.97 0.9728 42.08 0.9723 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

20a,b,c 72.0 71.4 71.7 71.4 72.5 88.1 71.4 0 0 43.35 1.0045 43.34 1.0011 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

21a,b,c 72.5 71.4 71.6 71.4 72.5 89.1 71.4 0 0 44.52 1.0313 44.55 1.0287 orange 8.380 7.890 8.010 8.170 5.190 6.410 0.510 29.91

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 10exit 2 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

69psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.2 72.8 72.9 72.7 72.9 76.9 71.9 0 0 24.11 0.5601 24.19 0.5602 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

2a,b,c 75.9 72.8 72.9 72.8 73.0 77.4 71.9 0 0 25.30 0.5875 25.30 0.5859 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

3a,b,c 76.0 72.9 73.0 72.8 73.1 77.9 71.9 0 0 36.32 0.6112 26.35 0.6101 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

4a,b,c 76.3 72.9 73.0 72.9 73.2 78.5 71.9 0 0 27.45 0.6374 27.51 0.6368 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

5a,b,c 76.3 72.9 73.0 72.8 73.2 79.0 71.9 0 0 28.70 0.6663 28.76 0.6659 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

6a,b,c 76.2 72.9 73.0 72.8 73.2 79.4 71.9 0 0 29.87 0.6935 29.91 0.6925 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

7a,b,c 76.2 72.9 73.0 72.7 73.2 80.0 71.9 0 0 31.03 0.7204 31.05 0.7189 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

8a,b,c 75.2 72.8 72.9 72.7 73.2 80.6 71.9 0 0 32.15 0.7462 32.20 0.7454 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

9a,b,c 75.3 72.8 73.0 72.7 73.3 81.3 71.9 0 0 33.43 0.7756 33.46 0.7745 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

10a,b,c 75.2 72.9 73.0 72.8 73.4 82.1 71.9 0 0 34.70 0.8055 34.75 0.8040 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

11a,b,c 75.7 72.9 73.0 72.8 73.4 83.0 71.9 0 0 35.99 0.8350 36.06 0.8340 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

12a,b,c 75.7 72.9 73.0 72.8 73.4 83.4 71.9 0 0 37.42 0.8679 37.32 0.8636 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

13a,b,c 75.9 72.8 73.0 72.8 73.4 83.7 71.9 0 0 38.62 0.8955 38.66 0.8940 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

14a,b,c 75.4 72.8 72.9 72.7 73.4 84.6 71.9 0 0 39.48 0.9156 39.54 0.9144 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

15a,b,c 75.1 72.8 72.9 72.7 73.4 85.4 71.9 0 0 40.78 0.9453 40.72 0.9414 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

16a,b,c 75.2 72.7 72.8 72.6 73.4 86.0 71.9 0 0 41.92 0.9717 41.87 0.9670 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

17a,b,c 75.2 72.7 72.8 72.6 73.4 86.6 71.9 0 0 43.07 0.9979 43.07 0.9953 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

18a,b,c 75.6 72.7 72.8 72.6 73.4 87.3 71.9 0 0 44.19 1.0235 44.14 1.0203 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

19a,b,c 75.1 72.6 72.8 72.6 73.4 87.8 71.9 0 0 45.30 1.0495 45.23 1.0442 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

20a,b,c 74.8 72.6 72.7 72.6 73.5 88.6 71.9 0 0 46.35 1.0735 46.30 1.0688 orange 12.25 11.62 11.89 11.91 7.61 9.41 0.78 29.92

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -42

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 10exit 2blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.2 67.3 67.7 67.3 69.2 74.0 70.8 0 0 27.26 0.6332 27.30 0.6324 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

2a,b,c 72.6 66.6 67.0 66.6 68.6 74.1 70.8 0 0 28.81 0.6692 28.89 0.6689 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

3a,b,c 73.0 66.4 66.7 66.4 68.4 74.5 70.8 0 0 30.25 0.7027 30.17 0.6989 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

4a,b,c 73.1 66.9 67.2 66.8 68.5 75.3 70.8 0 0 31.94 0.7417 32.02 0.7415 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

5a,b,c 73.5 67.3 67.6 67.2 68.7 76.0 70.8 0 0 33.53 0.7785 33.61 0.7782 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

6a,b,c 73.4 67.8 68.0 67.7 69.0 76.9 70.8 0 0 35.10 0.8146 35.04 0.8112 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

7a,b,c 73.2 68.2 68.4 68.0 69.2 77.9 70.8 0 0 36.53 0.8479 36.55 0.8459 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

8a,b,c 73.9 68.7 68.9 68.5 69.6 78.9 70.8 0 0 38.07 0.8835 38.13 0.8821 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

9a,b,c 74.1 68.9 69.1 68.8 69.8 79.9 70.8 0 0 39.59 0.9182 39.63 0.9169 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

10a,b,c 74.3 69.2 69.4 69.1 70.0 80.8 70.8 0 0 41.11 0.9535 41.11 0.9508 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

11a,b,c 73.9 69.6 69.8 69.5 70.3 81.7 70.8 0 0 42.60 0.9881 42.59 0.9849 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

12a,b,c 73.8 70.0 70.1 69.8 70.6 82.8 70.8 0 0 44.00 1.0210 44.13 1.0199 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

13a,b,c 74.3 70.3 70.4 70.1 70.9 84.0 70.8 0 0 45.48 1.0540 45.39 1.0489 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

14a,b,c 74.3 70.6 70.7 70.4 71.1 84.5 70.8 0 0 46.60 1.0791 46.59 1.0763 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

15a,b,c 74.4 70.7 70.8 70.5 71.3 85.6 70.8 0 0 47.41 1.0983 47.53 1.0976 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

16a,b,c 75.1 71.0 71.1 70.8 71.6 86.6 70.8 0 0 48.64 1.1254 48.64 1.1231 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

17a,b,c 75.4 71.3 71.4 71.1 71.9 87.4 70.8 0 0 49.96 1.1565 49.83 1.1498 orange 15.19 14.56 14.82 14.9 9.45 11.89 0.99 29.93

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -43

11crossover holes-9 exit holes, staggered arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0degree 11 cross-over holes---9 exti holes

TE slot Arrangement : staggered

Experimentalist : Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 05 / 08 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 69.5 70.5 70.7 72.2 0.255 0.237 0.243 0.247 0.133 0.181 water 29.91 0.02 70.5 0

10 69.5 70.5 70.7 72.2 0.431 0.399 0.412 0.416 0.24 0.311 water 29.91 0.029 70.5 0

15 69.5 70.5 70.7 72.2 0.638 0.598 0.612 0.618 0.382 0.472 water 29.91 0.04 70.5 0

20 69.5 70.5 70.7 72.2 0.888 0.834 0.852 0.856 0.521 0.657 water 29.91 0.052 70.5 0

25 69.5 70.5 70.7 72.2 2.9 2.71 2.75 2.81 1.78 2.24 orange 29.91 0.08 70.5 0

30 69.5 70.5 70.7 72.2 3.6 3.39 3.43 3.49 2.2 2.74 orange 29.91 0.22 70.5 0

40 69.5 70.5 70.7 72.2 5.46 5.1 5.21 5.31 3.39 4.17 orange 29.91 0.33 70.5 0

50 69.5 70.5 70.7 72.2 7.48 7.02 7.19 7.26 4.59 5.71 orange 29.91 0.34 70.5 0

60 69.5 70.5 70.7 72.2 9.84 9.31 9.5 9.59 6.09 7.61 orange 29.91 0.7 70.5 0

70 69.5 70.5 70.7 72.2 12.25 11.62 11.89 11.91 7.61 9.41 orange 29.91 0.78 70.5 0

80 69.5 70.5 70.7 72.2 15.19 14.56 14.82 14.9 9.45 11.89 orange 29.91 0.99 70.5 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover9exits 3blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.3 70.6 70.8 70.5 71.3 77.4 71.5 0 0 19.17 0.4452 19.07 0.4417 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

2a,b,c 69.6 70.6 70.8 70.5 71.3 79.0 71.5 0 0 19.87 0.4614 19.87 0.4598 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

3a,b,c 69.5 70.6 70.8 70.5 71.4 80.0 71.5 0 0 20.56 0.4776 20.60 0.4768 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

4a,b,c 69.6 70.6 70.7 70.5 71.4 80.7 71.5 0 0 21.46 0.4985 21.41 0.4954 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

5a,b,c 69.3 70.6 70.8 70.5 71.4 81.8 71.5 0 0 22.34 0.5186 22.34 0.5170 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

6a,b,c 69.1 70.6 70.7 70.5 71.5 82.9 71.5 0 0 23.13 0.5372 23.05 0.5334 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

7a,b,c 69.1 70.5 70.7 70.6 71.5 83.5 71.5 0 0 23.81 0.5526 23.84 0.5514 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

8a,b,c 68.9 70.6 70.7 70.5 71.5 84.8 71.5 0 0 24.58 0.5707 24.64 0.5699 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

9a,b,c 69.3 70.5 70.7 70.5 71.6 85.3 71.5 0 0 25.45 0.5907 25.39 0.5874 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

10a,b,c 69.2 70.5 70.7 70.5 71.6 86.8 71.5 0 0 26.24 0.6090 26.32 0.6086 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

11a,b,c 68.7 70.5 70.7 70.5 71.6 87.5 71.5 0 0 27.00 0.6267 27.03 0.6250 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

12a,b,c 68.8 70.4 70.6 70.4 71.6 88.6 71.5 0 0 27.90 0.6472 27.95 0.6461 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

13a,b,c 688.0 70.4 70.6 70.4 71.6 89.8 71.5 0 0 28.66 0.6649 28.65 0.6623 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

14a,b,c 68.6 70.4 70.6 70.4 71.6 90.9 71.5 0 0 29.46 0.6836 29.47 0.6812 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

15a,b,c 68.8 70.4 70.6 70.4 71.6 92.3 71.5 0 0 30.21 0.7009 30.23 0.6990 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

16a,b,c 68.8 70.4 70.6 70.4 71.6 93.5 71.5 0 0 31.09 0.7211 31.11 0.7190 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

17a,b,c 68.6 70.3 70.5 70.4 71.7 94.4 71.5 0 0 31.90 0.7397 31.87 0.7363 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

18a,b,c 68.7 70.3 70.5 70.4 71.7 95.6 71.5 0 0 32.71 0.7583 32.69 0.7551 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

19a,b,c 69.0 70.3 70.5 70.3 71.7 97.2 71.5 0 0 33.35 0.7733 33.40 0.7713 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

20a,b,c 68.9 70.3 70.5 70.3 71.8 97.9 71.5 0 0 34.36 0.7966 34.19 0.7895 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

21a,b,c 69.1 70.3 70.5 70.3 71.7 99.6 71.5 0 0 35.11 0.8140 35.18 0.8122 water 0.688 0.684 0.665 0.669 0.427 0.560 0.047 29.95

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -44

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover9exit 3 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.3 70.7 70.9 70.7 71.3 76.4 71.0 0 0 20.59 0.4783 20.63 0.4777 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

2a,b,c 71.3 70.9 71.0 70.8 71.4 77.7 71.0 0 0 21.52 0.4997 21.57 0.4993 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

3a,b,c 71.3 70.9 71.1 70.9 71.5 78.5 71.0 0 0 22.48 0.5221 22.39 0.5183 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

4a,b,c 71.8 71.1 71.3 71.0 71.6 79.1 71.0 0 0 23.27 0.5405 23.29 0.5388 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

5a,b,c 71.7 71.2 71.3 71.1 71.7 79.8 71.0 0 0 24.24 0.5628 24.17 0.5595 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

6a,b,c 71.8 71.2 71.4 71.1 71.9 80.8 71.0 0 0 25.16 0.5843 25.05 0.5797 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

7a,b,c 71.2 71.3 71.4 71.1 71.9 81.5 71.0 0 0 25.98 0.6033 26.01 0.6021 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

8a,b,c 71.8 71.2 71.3 71.1 71.9 82.3 71.0 0 0 26.92 0.6249 26.89 0.6221 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

9a,b,c 71.0 71.2 71.3 71.1 71.9 83.1 71.0 0 0 27.92 0.6480 27.94 0.6464 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

10a,b,c 71.6 71.1 71.2 71.0 71.9 83.8 71.0 0 0 28.71 0.6666 28.74 0.6650 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

11a,b,c 71.1 71.1 71.2 70.9 71.9 84.7 71.0 0 0 29.61 0.6872 29.66 0.6859 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

12a,b,c 71.3 71.0 71.2 70.9 71.9 85.2 71.0 0 0 30.59 0.7098 30.65 0.7088 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

13a,b,c 71.1 71.0 71.2 70.9 71.9 86.3 71.0 0 0 31.52 0.7316 31.62 0.7310 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

14a,b,c 70.8 70.8 71.0 70.8 71.8 87.2 71.0 0 0 32.51 0.7544 32.59 0.7533 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

15a,b,c 70.7 70.8 71.0 70.8 71.8 88.1 71.0 0 0 33.55 0.7784 33.51 0.7743 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

16a,b,c 71.0 70.8 71.0 70.7 71.8 89.5 71.0 0 0 34.75 0.8059 34.64 0.8004 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

17a,b,c 70.3 70.7 70.9 70.7 71.8 90.1 71.0 0 0 35.34 0.8196 35.39 0.8175 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

18a,b,c 70.4 70.8 71.0 70.7 71.8 90.9 71.0 0 0 36.62 0.8489 36.62 0.8455 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

19a,b,c 70.5 70.7 70.9 70.7 71.8 92.1 71.0 0 0 37.55 0.8705 37.59 0.8677 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

20a,b,c 70.5 70.7 70.9 70.7 71.8 93.4 71.0 0 0 38.46 0.8913 38.42 0.8875 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

21a,b,c 70.1 70.7 70.9 70.7 71.9 94.7 71 0 0 39.54 0.9161 39.47 0.9110 orange 3.610 3.390 3.450 3.510 2.290 2.990 0.280 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 9exit 3 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.6 70.4 70.6 70.3 71.4 76.2 71.8 0 0 22.35 0.5193 22.42 0.5190 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

2a,b,c 69.9 70.2 70.5 70.3 71.3 76.8 71.8 0 0 23.35 0.5424 23.30 0.5396 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

3a,b,c 70.3 70.2 70.5 70.2 71.3 77.3 71.8 0 0 24.34 0.5652 24.42 0.5653 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

4a,b,c 70.5 70.2 70.4 70.2 71.3 77.9 71.8 0 0 25.42 0.5903 25.42 0.5886 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

5a,b,c 70.5 70.2 70.5 70.2 71.3 78.6 71.8 0 0 26.29 0.6105 26.35 0.6101 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

6a,b,c 70.6 70.3 70.5 70.2 71.3 79.3 71.8 0 0 27.36 0.6354 27.42 0.6347 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

7a,b,c 71.2 70.3 70.5 70.2 71.3 79.9 71.8 0 0 28.35 0.6853 28.38 0.6568 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

8a,b,c 70.7 70.3 70.6 70.2 71.3 80.6 71.8 0 0 29.47 0.6842 29.42 0.6810 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

9a,b,c 70.7 70.3 70.6 70.3 71.3 81.5 71.8 0 0 30.51 0.7082 30.55 0.7069 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

10a,b,c 70.4 70.3 70.6 70.3 71.3 82.1 71.8 0 0 31.62 0.7338 31.67 0.7325 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

11a,b,c 70.9 70.4 70.6 70.4 71.4 82.9 71.8 0 0 32.73 0.7597 32.73 0.7570 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

12a,b,c 70.7 70.4 70.6 70.3 71.4 83.9 71.8 0 0 33.70 0.7820 33.72 0.7801 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

13a,b,c 70.8 70.4 70.6 70.3 71.4 84.5 71.8 0 0 34.87 0.8089 34.89 0.8068 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

14a,b,c 71.0 70.4 70.6 70.4 71.4 85.4 71.8 0 0 35.93 0.8337 35.85 0.8287 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

15a,b,c 70.5 70.4 70.6 70.4 71.4 86.2 71.8 0 0 36.92 0.8560 36.80 0.8507 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

16a,b,c 70.5 70.4 70.6 70.3 71.5 86.9 71.8 0 0 37.92 0.8793 37.79 0.8735 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

17a,b,c 71.2 70.4 70.6 70.4 71.5 88.2 71.8 0 0 38.94 0.9029 38.99 0.9008 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

18a,b,c 71.2 70.4 70.6 70.4 71.5 89.0 71.8 0 0 40.01 0.9277 40.01 0.9240 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

19a,b,c 70.9 70.4 70.6 70.4 71.6 89.8 71.8 0 0 41.23 0.9555 41.09 0.9487 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

20a,b,c 70.6 70.4 70.6 70.4 71.6 90.8 71.8 0 0 42.31 0.9807 42.24 0.9752 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

21a,b,c 71.1 70.4 70.6 70.3 71.6 91.8 71.8 0 0 43.45 1.0064 43.33 1.0000 orange 6.260 5.910 6.010 6.110 3.990 5.190 0.410 30.00

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -45

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 9exit 3blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.4 71.0 71.3 71.0 71.8 76.4 69.6 0 0 24.05 0.5585 24.12 0.5585 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

2a,b,c 72.3 71.0 71.2 71.0 71.8 77.3 69.6 0 0 25.09 0.5827 25.15 0.5824 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

3a,b,c 72.6 71.1 71.2 71.0 71.8 77.8 69.6 0 0 26.27 0.6100 26.36 0.6102 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

4a,b,c 72.2 71.0 71.2 71.0 71.8 78.2 69.6 0 0 27.41 0.6366 27.51 0.6369 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

5a,b,c 71.3 70.9 71.1 70.8 71.7 79.4 69.6 0 0 28.60 0.6637 28.62 0.6623 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

6a,b,c 71.5 70.6 70.9 70.6 73.3 79.7 69.6 0 0 29.78 0.6913 29.82 0.6902 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

7a,b,c 71.7 70.7 70.9 70.7 71.6 80.2 69.6 0 0 30.94 0.7183 31.02 0.7179 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

8a,b,c 71.9 70.7 70.9 70.7 71.6 80.8 69.6 0 0 32.14 0.7459 32.11 0.7430 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

9a,b,c 71.5 70.7 71.0 70.7 71.6 81.6 69.6 0 0 33.24 0.7718 33.29 0.7699 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

10a,b,c 71.3 70.7 70.9 70.7 71.7 82.1 69.6 0 0 34.44 0.7991 34.38 0.7956 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

11a,b,c 71.6 70.8 71.0 70.7 71.7 82.8 69.6 0 0 35.44 0.8222 35.53 0.8217 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

12a,b,c 72.4 70.9 71.0 70.8 71.8 83.7 69.6 0 0 36.53 0.8474 36.60 0.8463 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

13a,b,c 71.3 70.7 70.9 70.7 71.7 84.5 69.6 0 0 37.64 0.8731 37.68 0.8716 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

14a,b,c 71.3 70.6 70.8 70.6 71.6 85.0 69.6 0 0 38.80 0.8999 38.86 0.8982 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

15a,b,c 71.8 70.6 70.8 70.6 71.7 86.0 69.6 0 0 39.90 0.9253 40.00 0.9243 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

16a,b,c 71.6 70.7 70.9 70.6 71.7 86.7 69.6 0 0 41.02 0.9512 41.00 0.9473 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

17a,b,c 71.3 70.8 70.9 70.7 71.8 87.3 69.6 0 0 42.13 0.9766 42.11 0.9726 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

18a,b,c 71.5 70.6 70.8 70.6 71.7 88.3 69.6 0 0 43.26 1.0023 43.33 1.0006 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

19a,b,c 71.6 70.6 70.8 70.6 71.7 88.8 69.6 0 0 44.32 1.0276 44.42 1.0256 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

20a,b,c 71.6 70.6 70.8 70.6 71.8 90.3 69.6 0 0 45.51 1.0541 45.47 1.0494 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

21a,b,c 71.2 70.4 70.7 70.4 71.7 90.8 69.6 0 0 46.62 1.0799 46.74 1.0784 orange 9.890 9.340 9.490 9.530 6.310 8.100 0.690 30.03

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 9exit 3 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

69psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.5 72.4 72.6 72.3 73.3 77.2 71.4 0 0 25.06 0.5823 25.08 0.5808 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

2a,b,c 74.4 72.7 72.9 72.6 73.6 78.0 71.4 0 0 26.46 0.6145 26.28 0.6086 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

3a,b,c 75.2 72.8 73.0 72.6 73.8 78.8 71.4 0 0 27.63 0.6416 27.64 0.6400 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

4a,b,c 74.3 72.8 73.0 72.7 73.9 79.3 71.4 0 0 28.78 0.6683 28.83 0.6676 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

5a,b,c 74.3 72.8 73.1 72.6 74.1 80.0 71.4 0 0 30.05 0.6979 30.17 0.6984 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

6a,b,c 75.4 73.0 73.1 72.9 74.1 80.7 71.4 0 0 31.26 0.7256 31.29 0.7243 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

7a,b,c 75.3 73.1 73.2 72.9 74.2 81.3 71.4 0 0 32.59 0.7564 32.52 0.7525 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

8a,b,c 74.4 73.0 73.2 72.9 74.2 82.0 71.4 0 0 33.85 0.7855 33.86 0.7835 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

9a,b,c 74.6 73.0 73.1 72.9 74.0 82.6 71.4 0 0 35.10 0.8144 35.01 0.8101 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

10a,b,c 74.5 72.9 73.0 72.8 73.7 83.3 71.4 0 0 36.42 0.8449 36.34 0.8405 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

11a,b,c 74.9 72.9 73.0 72.8 73.5 83.9 71.4 0 0 37.52 0.8704 37.61 0.8697 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

12a,b,c 74.2 72.6 72.7 72.5 73.2 84.7 71.4 0 0 38.93 0.9028 38.94 0.9003 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

13a,b,c 74.5 72.6 72.7 72.5 72.9 85.3 71.4 0 0 40.30 0.9346 40.16 0.9280 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

14a,b,c 73.8 72.5 72.7 72.4 72.7 85.9 71.4 0 0 41.27 0.9573 41.49 0.9589 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

15a,b,c 73.6 72.3 72.5 72.2 72.3 86.5 71.4 0 0 42.74 0.9907 42.80 0.9890 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

16a,b,c 74.0 72.2 72.4 72.1 72.1 87.4 71.4 0 0 44.09 1.0214 44.09 1.0182 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

17a,b,c 74.3 72.2 72.4 72.1 71.8 88.3 71.4 0 0 45.26 1.0482 45.28 1.0457 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

18a,b,c 73.6 72.1 72.2 72.0 71.5 88.7 71.4 0 0 46.42 1.0749 46.51 1.0737 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

19a,b,c 73.6 72.0 72.2 72.0 71.6 89.8 71.4 0 0 47.78 1.1064 47.73 1.1016 orange 14.28 13.62 13.82 13.98 9.26 11.81 0.94 30.08

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -46

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 9exit 3blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.9 66.9 67.2 66.9 68.3 73.1 74.4 0 0 26.86 0.6238 26.96 0.6247 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

2a,b,c 73.8 67.2 67.5 67.1 68.3 73.9 74.4 0 0 28.42 0.6601 28.49 0.6598 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

3a,b,c 74.2 68.0 68.2 67.8 68.8 74.8 74.4 0 0 30.09 0.6989 30.14 0.6981 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

4a,b,c 73.9 68.4 68.6 68.3 69.2 75.7 74.4 0 0 31.57 0.7333 31.52 0.7302 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

5a,b,c 73.9 68.8 68.9 68.6 69.4 76.6 74.4 0 0 33.10 0.7685 33.12 0.7668 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

6a,b,c 73.8 69.2 69.3 69.0 69.7 77.6 74.4 0 0 34.56 0.8023 34.48 0.7984 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

7a,b,c 74.7 69.7 69.8 69.6 70.1 78.8 74.4 0 0 36.03 0.8356 36.13 0.8360 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

8a,b,c 74.6 69.9 70.1 69.8 70.4 79.7 74.4 0 0 37.55 0.8714 37.60 0.8700 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

9a,b,c 74.3 70.2 70.3 70.1 70.6 80.6 74.4 0 0 39.04 0.9058 39.11 0.9048 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

10a,b,c 74.6 70.4 70.6 70.3 70.9 81.5 74.4 0 0 40.65 0.9427 40.61 0.9393 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

11a,b,c 74.5 70.8 70.9 70.6 71.3 82.9 74.4 0 0 42.14 0.9772 42.07 0.9725 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

12a,b,c 74.1 70.9 71.1 70.8 71.4 83.8 74.4 0 0 43.61 1.0109 43.71 1.0101 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

13a,b,c 74.5 71.0 71.1 70.9 71.6 84.8 74.4 0 0 44.95 1.0417 45.13 1.0426 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

14a,b,c 74.3 71.1 71.2 71.0 71.7 85.6 74.4 0 0 46.04 1.0670 46.25 1.0682 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

15a,b,c 74.3 71.3 71.4 71.1 72.0 86.5 74.4 0 0 47.12 1.0917 47.22 1.0904 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

16a,b,c 74.7 71.5 71.6 71.4 72.2 87.4 74.4 0 0 47.95 1.1104 48.03 1.1091 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

17a,b,c 74.8 71.5 71.6 71.4 72.3 88.2 74.4 0 0 49.01 1.1349 49.16 1.1341 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

18a,b,c 74.8 71.6 71.6 71.4 72.3 88.9 74.4 0 0 50.21 1.1627 50.15 1.1574 orange 17.62 16.96 17.32 17.28 11.5 14.78 1.26 30.08

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -47

11crossover holes-8 exit holes, staggered arrangement, 0 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" Cross-Over Hole Angle : 0 degree 11 cross-over holes---12 exit holes

TE slot Arrangement : staggered

Experimentalist : Bleed Valve : closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date: 05 / 08 / 2012

COLD TEST

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ΔPjet Tjet ΔPorifice

5 71.8 71 71.2 72.6 0.202 0.174 0.19 0.195 0.086 0.086 water 29.81 0.018 71.4 0

10 71.8 71 71.2 72.6 0.344 0.317 0.324 0.332 0.172 0.172 water 29.81 0.031 71.4 0

15 71.8 71 71.2 72.6 0.496 0.455 0.466 0.477 0.256 0.257 water 29.81 0.045 71.4 0

20 71.8 71 71.2 72.6 0.694 0.646 0.658 0.667 0.377 0.377 water 29.81 0.066 71.4 0

25 71.8 71 71.2 72.6 0.99 0.921 0.942 0.947 0.534 0.534 water 29.81 0.087 71.4 0

30 71.8 71 71.2 72.6 2.91 2.69 2.71 2.8 1.7 1.65 orange 29.81 0.28 71.4 0

40 71.8 71 71.2 72.6 4.31 4.01 4.19 4.19 2.49 2.49 orange 29.81 0.38 71.4 0

50 71.8 71 71.2 72.6 5.98 5.58 5.73 5.79 3.47 3.41 orange 29.81 0.51 71.4 0

60 71.8 71 71.2 72.6 7.93 7.42 7.61 7.71 4.61 4.59 orange 29.81 0.7 71.4 0

70 71.8 71 71.2 72.6 10.11 9.45 9.68 9.72 5.79 5.83 orange 29.81 0.9 71.4 0

80 71.8 71 71.2 72.6 12.31 11.44 11.81 11.91 7.01 7.14 orange 29.81 1.11 71.4 0

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover8exits 4blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.9 71.1 71.2 71.1 71.9 77.8 71.4 0 0 18.08 0.4198 18.02 0.4169 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

2a,b,c 71.2 71.1 71.2 71.1 71.6 78.4 71.4 0 0 18.74 0.4350 18.74 0.4338 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

3a,b,c 71.1 71.1 71.2 71.1 71.5 79.4 71.4 0 0 19.49 0.4524 19.51 0.4516 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

4a,b,c 71.0 71.1 71.2 71.1 71.5 80.2 71.4 0 0 20.26 0.4703 20.36 0.4709 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

5a,b,c 71.1 71.1 71.3 70.9 71.4 81.1 71.4 0 0 21.20 0.4922 21.15 0.4896 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

6a,b,c 71.0 71.2 71.3 71.2 71.3 82.2 71.4 0 0 22.08 0.5125 22.05 0.5102 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

7a,b,c 70.9 71.2 71.3 71.1 71.4 82.9 71.4 0 0 22.94 0.5324 22.89 0.5295 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

8a,b,c 70.9 71.3 71.4 71.3 71.5 84.4 71.4 0 0 23.75 0.5514 23.83 0.5512 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

9a,b,c 71.3 71.3 71.5 71.2 71.6 85.2 71.4 0 0 24.67 0.5726 24.63 0.5696 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

10a,b,c 70.8 71.4 71.5 71.4 71.7 86.9 71.4 0 0 25.47 0.5911 25.39 0.5871 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

11a,b,c 70.8 71.5 71.6 71.4 71.7 87.8 71.4 0 0 26.27 0.6096 26.28 0.6078 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

12a,b,c 70.9 71.6 71.7 71.5 71.8 89.0 71.4 0 0 27.08 0.6285 27.12 0.6271 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

13a,b,c 70.6 71.5 71.7 71.4 71.9 90.3 71.4 0 0 27.90 0.6474 27.83 0.6433 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

14a,b,c 70.6 71.5 71.7 71.5 71.8 91.9 71.4 0 0 28.63 0.6641 28.70 0.6633 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

15a,b,c 70.5 71.5 71.7 71.4 71.8 92.8 71.4 0 0 29.60 0.6869 29.59 0.6838 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

16a,b,c 71.0 71.4 71.6 71.4 71.6 94.3 71.4 0 0 30.60 0.7097 30.52 0.7053 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

17a,b,c 70.8 71.4 71.6 71.4 71.6 96.0 71.4 0 0 31.42 0.7291 31.40 0.7254 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

18a,b,c 70.2 71.3 71.5 71.3 71.6 96.7 71.4 0 0 32.13 0.7450 32.16 0.7429 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

19a,b,c 70.3 71.4 71.6 71.4 71.8 98.2 71.4 0 0 32.93 0.7633 32.90 0.7595 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

20a,b,c 70.5 71.3 71.6 71.2 71.8 99.2 71.4 0 0 33.65 0.7800 33.59 0.7755 water 0.842 0.811 0.816 0.827 0.567 0.732 0.051 30.11

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -48

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover8exit 4 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.9 71.8 72.0 71.7 72.0 77.2 70.4 0 0 20.48 0.4757 20.50 0.4749 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

2a,b,c 72.3 71.9 72.1 71.9 72.2 78.2 70.4 0 0 21.45 0.4982 21.41 0.4956 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

3a,b,c 72.5 71.9 72.1 71.8 72.2 78.9 70.4 0 0 22.34 0.5191 22.21 0.5157 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

4a,b,c 72.3 71.9 72.0 71.8 72.2 79.7 70.4 0 0 23.21 0.5390 23.27 0.5385 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

5a,b,c 72.4 71.8 72.0 71.7 72.2 80.6 70.4 0 0 24.10 0.5596 24.19 0.5600 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

6a,b,c 71.8 71.7 71.9 71.7 72.2 81.0 70.4 0 0 25.03 0.5810 24.97 0.5780 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

7a,b,c 71.4 71.8 71.9 71.7 72.3 81.8 70.4 0 0 25.90 0.6012 25.95 0.6005 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

8a,b,c 72.0 71.8 71.9 71.7 72.3 82.6 70.4 0 0 26.88 0.6239 26.83 0.6207 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

9a,b,c 71.9 71.6 71.8 71.7 72.3 83.3 70.4 0 0 27.74 0.6440 27.74 0.6419 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

10a,b,c 71.6 71.4 71.6 71.5 72.2 83.9 70.4 0 0 28.61 0.6636 28.68 0.6637 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

11a,b,c 71.1 71.5 71.7 71.5 72.3 84.8 70.4 0 0 29.64 0.6878 29.64 0.6855 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

12a,b,c 70.9 71.5 71.6 71.4 72.2 85.7 70.4 0 0 30.49 0.7074 30.51 0.7056 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

13a,b,c 70.7 71.3 71.5 71.3 72.2 86.3 70.4 0 0 31.40 0.7282 31.35 0.7248 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

14a,b,c 70.8 71.2 71.4 71.3 72.2 87.5 70.4 0 0 32.25 0.7483 32.26 0.7459 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

15a,b,c 70.3 71.2 71.3 71.2 72.2 88.2 70.4 0 0 33.25 0.7712 33.23 0.7682 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

16a,b,c 70.3 71.1 71.3 71.1 72.2 89.1 70.4 0 0 34.17 0.7926 34.21 0.7907 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

17a,b,c 70.8 71.0 71.2 71.1 72.1 90.2 70.4 0 0 35.31 0.8188 35.38 0.8174 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

18a,b,c 70.3 71.0 71.2 71.0 72.1 91.0 70.4 0 0 36.37 0.8434 36.43 0.8413 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

19a,b,c 70.0 70.9 71.1 71.0 72.1 92.0 70.4 0 0 37.45 0.8681 37.39 0.8634 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

20a,b,c 69.9 70.9 71.0 70.9 72.1 93.4 70.4 0 0 38.56 0.8938 38.64 0.8921 orange 4.700 4.490 4.580 4.610 3.230 4.110 0.280 30.09

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 8exit 4 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/08/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.1 72.1 72.2 72.0 72.3 76.7 70.8 0 0 21.90 0.5088 21.89 0.5068 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

2a,b,c 74.0 72.3 72.4 72.3 72.6 77.6 70.8 0 0 22.83 0.5301 22.85 0.5289 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

3a,b,c 73.8 72.3 72.5 72.2 72.9 78.2 70.8 0 0 23.29 0.5527 23.65 0.5475 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

4a,b,c 73.8 72.5 72.6 72.5 73.1 78.9 70.8 0 0 24.54 0.5698 24.49 0.5670 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

5a,b,c 74.1 72.6 72.6 72.5 73.3 79.5 70.8 0 0 25.42 0.5903 25.43 0.5886 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

6a,b,c 73.7 72.7 72.7 72.6 73.4 80.2 70.8 0 0 26.35 0.6117 26.33 0.6092 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

7a,b,c 73.9 72.6 72.7 72.6 73.4 80.9 70.8 0 0 27.26 0.6329 27.31 0.6318 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

8a,b,c 73.9 72.7 72.8 72.7 73.2 81.6 70.8 0 0 28.18 0.6540 28.18 0.6525 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

9a,b,c 73.4 72.6 72.7 72.5 73.0 82.3 70.8 0 0 29.08 0.6749 29.11 0.6736 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

10a,b,c 73.3 72.5 72.6 72.4 72.6 82.8 70.8 0 0 29.99 0.6962 30.07 0.6954 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

11a,b,c 73.2 72.3 72.4 72.3 72.3 83.4 70.8 0 0 30.96 0.7184 30.97 0.7164 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

12a,b,c 72.6 72.3 72.4 72.2 72.0 84.1 70.8 0 0 31.80 0.7380 31.93 0.7386 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

13a,b,c 72.7 72.1 72.2 72.0 71.8 84.9 70.8 0 0 32.72 0.7593 32.73 0.7570 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

14a,b,c 72.6 72.0 72.1 71.9 71.6 85.5 70.8 0 0 33.57 0.7787 33.63 0.7774 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

15a,b,c 72.2 71.9 72.1 71.8 71.6 86.3 70.8 0 0 34.56 0.8017 34.59 0.7997 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

16a,b,c 72.0 71.8 72.0 71.7 71.5 86.8 70.8 0 0 35.60 0.8257 35.57 0.8221 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

17a,b,c 72.0 71.7 71.9 71.7 71.4 87.8 70.8 0 0 36.60 0.8488 36.55 0.8446 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

18a,b,c 72.1 71.6 71.9 71.6 71.3 88.5 70.8 0 0 37.50 0.8704 37.55 0.8674 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

19a,b,c 72.3 71.6 71.8 71.6 71.5 89.3 70.8 0 0 38.98 0.9040 38.89 0.8983 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

20a,b,c 72.0 71.6 71.7 71.5 71.6 90.3 70.8 0 0 39.97 0.9260 39.96 0.9226 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

21a,b,c 72.2 71.5 71.7 71.5 71.7 91.2 70.8 0 0 41.01 0.9505 40.95 0.9454 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

22a,b,c 71.8 71.5 71.7 71.4 71.8 92.3 70.8 0 0 41.88 0.9703 41.83 0.9655 orange 7.890 7.590 7.590 7.690 5.370 6.880 0.430 29.98

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -49

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 8exit 4 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/07/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.5 72.6 72.7 72.5 72.7 76.7 69.7 0 0 23.04 0.5352 23.13 0.5356 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

2a,b,c 75.6 72.7 72.8 72.6 72.8 77.4 69.7 0 0 24.18 0.5616 24.16 0.5595 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

3a,b,c 74.8 72.7 72.8 72.7 72.9 78.0 69.7 0 0 25.19 0.5849 25.14 0.5819 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

4a,b,c 75.3 72.9 73.0 72.8 73.1 78.7 69.7 0 0 26.15 0.6073 26.18 0.6064 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

5a,b,c 75.3 72.9 73.0 72.8 73.1 79.3 69.7 0 0 27.16 0.6307 27.20 0.6296 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

6a,b,c 74.8 72.9 73.0 72.8 73.1 79.9 69.7 0 0 28.13 0.6545 28.23 0.6533 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

7a,b,c 75.1 72.8 72.9 72.7 73.1 80.5 69.7 0 0 29.17 0.6772 29.13 0.6738 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

8a,b,c 74.1 72.7 72.9 72.7 73.1 81.1 69.7 0 0 30.24 0.7017 30.15 0.6976 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

9a,b,c 74.7 72.7 72.8 72.6 73.1 81.6 69.7 0 0 31.09 0.7217 31.14 0.7205 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

10a,b,c 74.1 72.8 72.9 72.7 73.3 82.4 69.7 0 0 32.22 0.7480 32.21 0.7449 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

11a,b,c 74.0 72.7 72.8 72.7 73.2 83.0 69.7 0 0 33.23 0.7712 33.18 0.7676 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

12a,b,c 73.4 72.4 72.6 72.4 73.1 83.4 69.7 0 0 34.28 0.7952 34.21 0.7920 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

13a,b,c 73.7 72.4 72.5 72.3 73.0 84.0 69.7 0 0 35.24 0.8176 35.29 0.8159 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

14a,b,c 73.5 72.3 72.4 72.3 73.0 84.8 69.7 0 0 36.34 0.8430 36.21 0.8373 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

15a,b,c 73.6 72.3 72.4 72.2 73.0 85.4 69.7 0 0 37.30 0.8650 37.31 0.8627 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

16a,b,c 73.8 72.2 72.3 72.1 73.0 86.3 69.7 0 0 38.28 0.8875 38.25 0.8843 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

17a,b,c 72.8 72.0 72.2 72.0 72.9 87.3 69.7 0 0 39.40 0.9133 39.39 0.9099 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

18a,b,c 73.3 71.9 72.1 71.9 72.9 87.9 69.7 0 0 40.56 0.9403 40.52 0.9361 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

19a,b,c 73.5 72.1 72.2 72.0 73.0 88.7 69.7 0 0 41.58 0.9635 41.64 0.9616 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

20a,b,c 73.7 72.1 72.2 72.1 73.0 89.5 69.7 0 0 42.80 0.9917 42.84 0.9894 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

21a,b,c 73.6 72.1 72.2 72.1 73.1 90.5 69.7 0 0 43.96 1.0184 43.74 1.0100 orange 11.610 11.200 11.390 11.480 8.010 10.250 0.670 29.94

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 8exit 4 blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/07/2012 Remarks : Camera is focused on the last four crossover holes

69psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72.3 69.0 69.3 69.0 70.0 74.4 70.6 0 0 23.99 0.5573 24.01 0.5561 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

2a,b,c 72.7 69.2 69.4 69.2 70.1 74.9 70.6 0 0 25.11 0.5833 25.11 0.5816 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

3a,b,c 73.1 69.5 69.7 69.4 70.3 75.4 70.6 0 0 26.34 0.6118 26.39 0.6110 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

4a,b,c 73.2 69.7 69.9 69.6 70.4 76.1 70.6 0 0 27.53 0.6394 27.61 0.6394 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

5a,b,c 73.1 69.9 70.1 69.8 70.6 76.8 70.6 0 0 28.76 0.6678 28.81 0.6668 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

6a,b,c 73.4 70.1 70.3 70.0 70.7 77.5 70.6 0 0 29.99 0.6961 30.00 0.6946 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

7a,b,c 73.3 70.2 70.4 70.1 70.9 78.1 70.6 0 0 31.25 0.7255 31.27 0.7239 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

8a,b,c 73.5 70.4 70.6 70.3 71.0 78.9 70.6 0 0 32.44 0.7530 32.45 0.7510 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

9a,b,c 74.1 70.5 70.7 70.4 71.1 79.6 70.6 0 0 33.63 0.7804 33.61 0.7777 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

10a,b,c 73.2 70.6 70.7 70.5 71.2 80.2 70.6 0 0 34.83 0.8083 34.90 0.8075 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

11a,b,c 73.5 70.6 70.9 70.6 71.3 81.1 70.6 0 0 36.02 0.8359 36.15 0.8361 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

12a,b,c 74.0 70.8 70.9 70.7 71.5 81.8 70.6 0 0 37.28 0.8644 37.23 0.8611 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

13a,b,c 73.8 70.8 71.0 70.7 71.5 82.6 70.6 0 0 38.39 0.8902 38.44 0.8887 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

14a,b,c 73.6 70.9 71.1 70.8 71.6 83.4 70.6 0 0 39.63 0.9191 39.71 0.9179 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

15a,b,c 73.8 71.0 71.2 70.9 71.8 84.1 70.6 0 0 40.85 0.9471 40.72 0.9412 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

16a,b,c 73.7 71.0 71.2 71.0 71.9 85.1 70.6 0 0 42.00 0.9735 42.01 0.9713 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

17a,b,c 74.1 71.1 71.2 71.0 71.9 85.7 70.6 0 0 43.23 1.0020 43.21 0.9979 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

18a,b,c 73.8 71.0 71.2 71.0 71.9 86.6 70.6 0 0 44.37 1.0281 44.48 1.0272 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

19a,b,c 73.8 71.0 71.2 71.0 72.0 87.6 70.6 0 0 45.26 1.0601 45.82 1.0577 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

20a,b,c 74.8 71.1 71.3 71.0 72.1 88.7 70.6 0 0 47.04 1.0896 47.01 1.0852 orange 17.200 16.590 16.770 16.910 11.790 15.060 1.000 29.88

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -50

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 0˚ 11crossover 8exit 4blocked

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:05/07/2012 Remarks : Camera is focused on the last four crossover holes

80 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.1 71.9 72.1 71.9 73.6 76.1 74.1 0 0 24.23 0.5629 24.13 0.5589 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

2a,b,c 74.9 71.7 71.8 71.7 73.8 76.5 74.1 0 0 25.33 0.5882 25.37 0.5876 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

3a,b,c 74.8 71.6 71.8 71.6 74.0 77.1 74.1 0 0 26.60 0.6177 26.58 0.6153 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

4a,b,c 74.3 71.7 71.9 71.7 74.0 77.6 74.1 0 0 27.96 0.6491 27.98 0.6479 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

5a,b,c 73.3 71.8 71.9 71.6 73.9 78.1 74.1 0 0 29.06 0.6750 29.06 0.6927 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

6a,b,c 72.0 71.2 71.4 71.1 72.8 78.6 74.1 0 0 30.59 0.7100 30.56 0.7073 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

7a,b,c 71.8 71.0 71.2 70.9 72.7 79.0 74.1 0 0 31.72 0.7367 31.74 0.7345 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

8a,b,c 71.7 70.9 71.1 70.8 72.5 79.4 74.1 0 0 33.04 0.7667 33.11 0.7667 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

9a,b,c 72.2 70.8 71.0 70.7 72.3 79.9 74.1 0 0 34.29 0.7957 34.22 0.7916 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

10a,b,c 71.8 70.8 71.0 70.7 72.1 80.4 74.1 0 0 35.66 0.8271 35.75 0.8272 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

11a,b,c 72.4 70.6 70.9 70.5 71.9 81.2 74.1 0 0 37.02 0.8588 37.05 0.8570 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

12a,b,c 72.6 70.7 70.9 70.6 71.9 81.9 74.1 0 0 38.34 0.8895 38.25 0.8847 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

13a,b,c 71.8 70.6 70.8 70.6 71.8 82.5 74.1 0 0 39.61 0.9188 39.53 0.9139 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

14a,b,c 72.2 70.7 70.9 70.6 71.8 83.2 74.1 0 0 40.87 0.9479 40.88 0.9449 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

15a,b,c 72.8 70.6 70.8 70.6 71.7 83.9 74.1 0 0 42.18 0.9780 42.20 0.9753 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

16a,b,c 72.6 70.6 70.9 70.5 71.7 84.8 74.1 0 0 43.67 1.0122 43.47 1.0045 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

17a,b,c 72.3 70.7 70.9 70.6 71.8 85.5 74.1 0 0 44.91 1.0401 44.95 1.0384 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

18a,b,c 73.1 70.8 71.0 70.7 72.1 86.4 74.1 0 0 46.30 1.0730 46.34 1.0702 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

19a,b,c 72.6 70.7 71.0 70.7 72.4 87.1 74.1 0 0 47.60 1.1027 47.61 1.0993 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

20a,b,c 72.7 70.8 71.1 70.7 72.8 88.4 74.1 0 0 49.16 1.1384 49.13 1.1336 orange 21.550 20.790 21.050 21.090 14.790 18.940 1.220 30.11

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -51

11crossover holes-12 exit holes, staggered arrangement, 5 degree tilt angle, no bleed

Lab: 165EC

0.32 " 11 cross-over holes---12 exit holes

"Hg

Pven Tven Tin1 Tin2 Tamb Pplen Psup1 Psup2 Psup3 Pend1 Pend2 Man. Liquid Pamb ∆Pjet Tjet DP,orifice

5psi 77.9 75.4 75.6 70.5 0.233 0.204 0.213 0.224 0.128 0.126 water 30.12 0.012 75.4 0

10psi 77.9 75.4 75.6 70.5 0.374 0.343 0.356 0.367 0.214 0.207 water 30.12 0.019 75.4 0

15psi 77.9 75.4 75.6 70.5 0.53 0.487 0.504 0.513 0.301 0.294 water 30.12 0.029 75.4 0

20psi 77.9 75.4 75.6 70.5 0.726 0.682 0.674 0.706 0.415 0.4 water 30.12 0.034 75.4 0

25psi 77.9 75.4 75.6 70.5 2.23 2.11 2.16 2.16 0.527 0.517 orange 30.12 0.042 75.4 0

30psi 77.9 75.4 75.6 70.5 2.88 2.69 2.75 2.79 0.69 0.66 orange 30.12 0.058 75.4 0

40psi 77.9 75.4 75.6 70.5 4.22 3.93 4.06 4.09 2.41 2.33 orange 30.12 0.19 71.6 0

50psi 77.9 75.4 75.6 70.5 5.84 5.48 5.62 5.67 3.35 3.21 orange 30.12 0.23 75.4 0

60psi 77.9 75.4 75.6 70.5 7.68 7.19 7.48 7.42 4.39 4.25 orange 30.12 0.3 75.4 0

70psi 77.9 75.4 75.6 70.5 9.86 9.22 9.45 9.55 5.62 5.44 orange 30.12 0.39 75.4 0

80psi 77.9 75.4 75.6 70.5 12.21 11.42 11.69 11.82 6.95 6.73 orange 30.12 0.43 75.4 0

Remarks: Micro-manometer(H₂O) readings should be multiplied by 2

Date: 12/04/2011

COLD TEST

Trailing -Edge Test Section With Cross-Over Jets

Critical Venturi Throat Diameter: Cross-Over Hole Angle: 5˚

TE slot Arrangement: staggered

Experimentalist : Xiao Huang Bleed Valve : closed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross12exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012 Remarks : Camera is focused on the last four crossover holes

13psi

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.7 72 72.4 72 72.6 83.7 70.5 0 0 22.26 0.5165 22.23 0.5142 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

2a,b,c 75.3 72.1 72.3 72 72.5 86.1 70.5 0 0 22.86 0.5302 22.85 0.528 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

3a,b,c 75.3 72.1 72.3 72.1 72.4 87.7 70.5 0 0 23.5 0.545 23.49 0.5428 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

4a,b,c 75.6 72.2 72.4 72.1 72.4 89.4 70.5 0 0 24.17 0.5606 24.14 0.5577 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

5a,b,c 75.6 72.3 72.5 72.2 72.4 90.8 70.5 0 0 24.73 0.5734 24.81 0.5732 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

6a,b,c 75.9 72.3 72.6 72.2 72.4 92 70.5 0 0 25.47 0.5909 25.5 0.5891 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

7a,b,c 75.7 72.5 72.7 72.4 72.4 93.7 70.5 0 0 26.05 0.6038 26.09 0.6027 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

8a,b,c 76 72.7 72.8 72.5 72.4 94.9 70.5 0 0 26.76 0.6201 26.77 0.6183 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

9a,a,b 76.4 72.7 72.9 72.5 72.4 96.4 70.5 0 0 27.16 0.6295 27.21 0.6283 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

10a,b,c 76.8 73 73 72.9 72.5 97.9 70.5 0 0 27.84 0.6451 27.8 0.6417 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

11a,b,c 77 73.1 73.2 72.9 72.5 99.1 70.5 0 0 28.57 0.662 28.39 0.655 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

12a,b,c 77.2 73.1 73.2 72.9 72.5 100.4 70.5 0 0 29.03 0.6725 29.08 0.6709 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

13a,b,c 77.4 73.1 73.2 72.9 72.5 102 70.5 0 0 29.61 0.6848 29.68 0.9849 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

14a,b,c 76.8 73.2 73.3 73 72.5 103.5 70.5 0 0 30.3 0.7016 30.24 0.6975 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

15a,b,c 77.2 73.2 73.4 72.9 72.5 105.2 70.5 0 0 30.91 0.7153 30.9 0.7128 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

16a,b,c 77.1 73.4 73.5 73.2 72.6 106.5 70.5 0 0 31.49 0.7287 31.55 0.728 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

17a,b,c 77.4 73.4 73.5 73.2 72.6 107.5 70.5 0 0 32.34 0.7488 32.36 0.7461 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

18a,b,c 77.9 73.4 73.5 73.2 72.6 109.5 70.5 0 0 33.02 0.7645 32.99 0.7604 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

19a,b,c 77.6 73.6 73.6 73.3 72.6 111.7 70.5 0 0 33.71 0.7801 33.71 0.7768 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

20a,b,c 77.4 73.6 73.7 73.4 72.6 113.6 70.5 0 0 34.49 0.7983 34.41 0.7929 water 0.386 0.351 0.361 0.361 0.173 0.167 0.029 29.98

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

A -52

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit staggered

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

26 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.1 70 70.1 70 70.5 82.6 70.8 0 0 24.43 0.5667 24.59 0.5685 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

2a,b,c 71.4 70.2 70.3 70.2 70.6 84.5 70.8 0 0 25.19 0.5843 25.25 0.5834 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

3a,b,c 71.9 70.3 70.5 70.2 70.8 86.3 70.8 0 0 25.88 0.6001 25.98 0.6006 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

4a,b,c 71.8 70.6 70.7 70.4 70.9 87.6 70.8 0 0 26.68 0.6187 26.63 0.6154 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

5a,b,c 72.1 70.6 70.9 70.5 71 89.4 70.8 0 0 27.3 0.6332 27.24 0.6293 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

6a,b,c 72.2 70.8 71 70.6 71.1 90.8 70.8 0 0 27.89 0.6467 27.98 0.6462 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

7a,b,c 72.2 71 71.1 70.7 71.2 92 70.8 0 0 28.57 0.6621 28.61 0.6607 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

8a,b,c 73 71 71.1 70.8 71.3 93.5 70.8 0 0 29.3 0.679 29.4 0.6788 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

9a,b,c 73 71.2 71.3 71 71.4 95.1 70.8 0 0 30.22 0.7002 30.3 0.6999 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

10a,b,c 72.8 71.2 71.4 71.1 71.4 96.8 70.8 0 0 31.07 0.7198 31.02 0.7166 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

11a,b,c 73 71.6 71.7 71.3 71.6 98.5 70.8 0 0 31.87 0.7383 31.77 0.733 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

12a,b,c 73.3 71.5 71.6 71.3 71.5 100.1 70.8 0 0 32.45 0.7517 32.53 0.7503 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

13a,b,c 73.4 71.6 71.8 71.4 71.7 101.9 70.8 0 0 33.32 0.7717 33.32 0.7685 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

14a,b,c 73.7 71.6 71.8 71.4 71.7 103.4 70.8 0 0 34.17 0.7913 33.98 0.784 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

15a,b,c 73.7 71.7 71.9 71.5 71.8 104.9 70.8 0 0 34.57 0.8002 34.59 0.7976 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

16a,b,c 73.7 71.8 72 71.6 71.9 105.9 70.8 0 0 35.48 0.8214 35.4 0.8151 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

17a,b,c 73.4 71.8 71.9 71.6 71.9 107.9 70.8 0 0 36.36 0.8415 36.29 0.8358 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

18a,b,c 73.6 71.9 72.1 71.8 71.9 109.9 70.8 0 0 37.16 0.8598 37.19 0.8557 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

19a,b,c 73.3 72.1 72.2 71.9 72 112.1 70.8 0 0 38.19 0.8832 38.22 0.8805 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

20a,b,c 73.8 72.1 72.2 71.9 72 114.2 70.8 0 0 39.29 0.9091 39.26 0.9046 orange 2.36 2.19 2.26 2.29 1.33 1.29 0.1 30.09

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ staggered 11cross-12exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:03/30/2012

40 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 73.8 71.6 71.8 71.6 72.1 83.8 70.8 0 0 25.76 0.5976 25.82 0.5968 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

2a,b,c 75.3 72 72.2 71.9 72.3 86.2 70.8 0 0 26.82 0.622 26.87 0.6211 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

3a,b,c 75.6 72.3 72.5 72.2 72.3 87.9 70.8 0 0 27.91 0.6469 27.9 0.6448 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

4a,b,c 76 72.7 72.8 72.5 72.5 89.7 70.8 0 0 28.97 0.6714 28.83 0.6658 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

5a,b,c 75.6 72.8 72.9 72.6 72.6 91 70.8 0 0 29.92 0.6935 29.94 0.6915 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

6a,b,c 75.4 72.9 73 72.7 72.6 93.2 70.8 0 0 30.82 0.7142 30.82 0.7117 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

7a,b,c 75.9 73.1 73.2 73 72.7 94.7 70.8 0 0 31.74 0.7353 31.88 0.736 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

8a,b,c 75.6 73.1 73.2 72.9 72.8 95.8 70.8 0 0 32.78 0.7588 32.76 0.7563 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

9a,b,c 75.7 73.2 73.3 73 72.8 97.3 70.8 0 0 33.6 0.7778 33.63 0.7761 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

10a,b,c 75.5 73.2 73.3 73 72.8 98.9 70.8 0 0 34.5 0.7989 34.45 0.795 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

11a,b,c 75.8 73.3 73.5 73.2 73 101 70.8 0 0 35.42 0.8201 35.44 0.8174 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

12a,b,c 75.7 73.3 73.4 73.2 73 102.4 70.8 0 0 36.35 0.8416 36.3 0.8371 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

13a,b,c 75.8 73.3 73.5 73.2 73 103.8 70.8 0 0 37.28 0.863 37.24 0.8586 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

14a,b,c 76.4 73.6 73.7 73.4 73.2 105.4 70.8 0 0 37.87 0.8759 37.69 0.8692 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

15a,b,c 76.6 73.6 73.7 73.5 73.2 106.5 70.8 0 0 38.29 0.8866 38.21 0.8813 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

16a,b,c 76.3 73.6 73.7 73.4 73.2 107.9 70.8 0 0 38.88 0.8995 38.88 0.8962 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

17a,b,c 76.4 73.6 73.8 73.5 73.3 108.8 70.8 0 0 39.53 0.9143 39.31 0.9055 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

18a,b,c 76.4 73.7 73.8 73.5 73.3 109.9 70.8 0 0 40.03 0.926 40.07 0.9234 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

19a,b,c 76.3 73.8 73.9 73.5 73.4 111.3 70.8 0 0 41.11 0.9501 41.03 0.945 orange 4.22 3.93 4.06 4.09 2.41 2.33 0.19 30.12

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -53

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

54 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.2 71.4 71.5 71.2 71.5 81.9 70.7 0 0 27.09 0.6283 27.12 0.6271 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

2a,b,c 75.2 71.8 71.9 71.7 71.7 83.3 70.7 0 0 28.02 0.6499 28.01 0.6478 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

3a,b,c 75.6 72.1 72.3 72 71.9 84.7 70.7 0 0 28.91 0.6708 28.92 0.6681 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

4a,b,c 75.7 72.5 72.5 72.3 72.1 86.1 70.7 0 0 29.84 0.692 29.8 0.6884 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

5a,b,c 75.9 72.7 72.8 72.5 72.3 87.3 70.7 0 0 30.77 0.7132 30.8 0.7117 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

6a,b,c 76.7 72.8 73 72.6 72.4 88.8 70.7 0 0 31.68 0.7343 31.64 0.7304 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

7a,b,c 76.4 73.2 73.3 73.1 72.6 90 70.7 0 0 32.59 0.7549 32.56 0.752 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

8a,b,c 76.4 73.3 73.4 73.1 72.7 91.2 70.7 0 0 33.47 0.7751 33.48 0.7729 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

9a,b,c 76.9 73.4 73.5 73.2 72.8 92.5 70.7 0 0 34.29 0.794 34.34 0.7926 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

10a,b,c 77.1 73.7 73.9 73.6 73 94 70.7 0 0 35.2 0.8154 35.18 0.8118 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

11a,b,c 77.1 74.1 74.2 73.8 73.3 95.6 70.7 0 0 36.19 0.8378 36.11 0.833 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

12a,b,c 77.3 74.2 74.3 73.9 73.5 97 70.7 0 0 37.05 0.8581 37 0.8533 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

13a,b,c 78.6 74.3 74.4 74.1 73.6 98.5 70.7 0 0 37.87 0.8764 37.85 0.8726 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

14a,b,c 78.1 74.6 74.6 74.3 73.7 99.9 70.7 0 0 38.87 0.8992 38.84 0.895 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

15a,b,c 79.1 74.7 74.8 74.4 73.8 101.4 70.7 0 0 39.82 0.9211 39.78 0.9169 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

16a,b,c 78.9 74.9 75 74.6 74 102.7 70.7 0 0 40.66 0.9404 40.61 0.9357 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

17a,b,c 79.4 75 75.1 74.8 74.1 104.4 70.7 0 0 41.6 0.9616 41.62 0.959 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

18a,b,c 78.7 75.1 75.2 75 74.2 105.7 70.7 0 0 42.51 0.9827 42.51 0.9792 orange 6.51 6.09 6.29 6.31 3.76 3.6 0.23 30.1

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11 cross 12 exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

69 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 78.6 73 73.1 73 73.3 81.7 70.3 0 0 28.03 0.6501 28.05 0.6484 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

2a,b,c 79.6 73.6 73.7 73.5 73.5 83 70.3 0 0 28.81 0.6678 28.77 0.665 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

3a,b,c 81 74.3 74.4 74.1 73.8 84.6 70.3 0 0 29.63 0.6872 29.69 0.6861 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

4a,b,c 80.3 74.9 75 74.7 74.2 85.7 70.3 0 0 30.5 0.7068 30.51 0.7046 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

5a,b,c 80.2 75.4 75.5 75.2 74.6 87.1 70.3 0 0 31.41 0.7281 31.6 0.7297 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

6a,b,c 80.6 75.5 75.6 75.3 74.7 88.3 70.3 0 0 32.42 0.7511 32.54 0.7508 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

7a,b,c 81.1 75.4 75.5 75.3 74.8 89 70.3 0 0 33.15 0.7681 33.12 0.7649 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

8a,b,c 81.7 75.1 75.2 75 74.8 89.6 70.3 0 0 34.02 0.7882 34.04 0.7862 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

9a,b,c 81.3 75.1 75.2 75 74.8 90.4 70.3 0 0 34.71 0.804 34.84 0.8042 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

10a,b,c 81.7 75.2 75.3 75.1 74.8 91.5 70.3 0 0 35.44 0.8206 35.3 0.8147 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

11a,b,c 82.1 75.1 75.3 75 74.7 93.2 70.3 0 0 36.21 0.8381 36.22 0.836 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

12a,b,c 82.1 75.4 75.4 75.1 74.8 94.3 70.3 0 0 36.99 0.856 37.11 0.8559 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

13a,b,c 82.4 75.5 75.6 75.5 75 95.6 70.3 0 0 37.75 0.8739 37.82 0.8723 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

14a,b,c 81.8 75.7 75.8 75.6 75 96.4 70.3 0 0 38.44 0.8892 38.49 0.8863 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

15a,b,c 81.9 75.8 75.9 75.7 75.1 97.3 70.3 0 0 39.37 0.9104 39.42 0.9086 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

16a,b,c 82.1 75.8 75.9 75.7 75.2 98.3 70.3 0 0 40.1 0.928 40.21 0.9273 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

17a,b,c 82.2 75.8 75.9 75.7 75.2 99.2 70.3 0 0 40.84 0.9445 40.69 0.9379 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

18a,b,c 82.4 76 76.1 75.9 75.3 100.2 70.3 0 0 41.41 0.9577 41.37 0.9537 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

19a,b,c 82.8 76.1 76.2 76 75.4 101 70.3 0 0 42.02 0.9713 42.03 0.9683 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

20a,b,c 83.3 76.1 76.3 76 75.4 102.1 70.3 0 0 42.77 0.9894 42.84 0.9867 orange 9.44 8.83 9.07 9.13 5.41 5.2 0.22 30.04

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -54

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross-12exit

cross

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/30/2012

80 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 79.5 75.2 75.4 75.2 75.2 82.3 70.5 0 0 29.07 0.674 29.12 0.6739 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

2a,b,c 82 72.4 72.7 72.7 74.2 83.1 70.5 0 0 29.9 0.6935 29.9 0.691 0.7122 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

3a,b,c 82.2 73 73.2 73.1 74 84.1 70.5 0 0 30.8 0.7144 30.82 0.7122 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

4a,b,c 82.6 73.9 74 73.9 74.3 85.6 70.5 0 0 31.61 0.7327 31.75 0.7337 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

5a,b,c 83.4 74.5 74.7 74.5 74.5 86.9 70.5 0 0 32.67 0.7576 32.65 0.7538 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

6a,b,c 83.6 75.2 75.2 75.1 74.8 88 70.5 0 0 33.77 0.7827 33.75 0.7788 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

7a,b,c 83.8 76 76.1 75.8 75.3 89.6 70.5 0 0 34.89 0.8078 34.71 0.8018 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

8a,b,c 84.2 76.4 76.5 76.3 75.5 90.8 70.5 0 0 35.68 0.8264 35.49 0.8191 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

9a,b,c 85 76.9 76.9 76.7 75.8 92 70.5 0 0 36.56 0.8465 36.55 0.8435 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

10a,b,c 85.2 77.4 77.5 77.2 76.2 93.4 70.5 0 0 37.54 0.8698 37.46 0.8645 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

11a,b,c 85.4 77.5 77.7 77.3 76.3 94.5 70.5 0 0 38.51 0.8919 38.44 0.8873 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

12a,b,c 85.6 78 78.1 77.8 76.6 95.7 70.5 0 0 39.04 0.9033 38.98 0.8968 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

13a,b,c 85.4 78.4 78.5 78.2 76.9 96.8 70.5 0 0 39.49 0.9137 39.5 0.9115 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

14a,b,c 85.8 78.7 78.7 78.4 77.2 97.7 70.5 0 0 40 0.9248 39.95 0.9205 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

15a,b,c 85.6 78.7 78.8 78.6 77.3 98.4 70.5 0 0 40.4 0.9348 40.4 0.9317 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

16a,b,c 86.2 79.1 79.1 78.8 77.5 99.1 70.5 0 0 41.07 0.9498 40.98 0.944 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

17a,b,c 85.7 79.3 79.4 79.1 77.8 100 70.5 0 0 41.89 0.9684 41.71 0.9618 orange 12.21 11.42 11.69 11.82 6.95 6.73 0.43 29.99

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -55

11crossover holes-10 exit holes, staggered arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:12/22/2011 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69 67.3 67.5 67.2 71.1 76.4 52 0 0 22.05 0.9972 22.05 0.9972 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

2a,b,c 69.6 67.4 67.5 67.3 71.4 76.8 52 0 0 22.72 1.0236 22.72 1.0236 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

3a,b,c 69.9 67.6 67.7 67.6 71.7 77.8 52 0 0 23.51 1.0582 23.51 1.0582 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

4a,b,c 70.8 67.8 67.9 67.7 72 78.4 52 0 0 24.25 1.0885 24.25 1.0885 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

5a,b,c 71.9 68.2 68.4 67.9 72.5 79.8 52 0 0 25.23 1.1285 25.23 1.1285 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

6a,b,c 73.5 68.4 68.5 68.3 72.6 80.5 52 0 0 26.09 1.166 26.09 1.166 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

7a,b,c 73.1 68.6 68.5 68.4 73 81.8 52 0 0 26.9 1.2018 26.9 1.2018 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

8a,b,c 74.1 68.8 68.8 68.6 73.2 82.2 52 0 0 27.64 1.2258 27.64 1.2258 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

9a,b,c 74 69.1 69 68.9 73.5 83.3 52 0 0 28.35 1.2611 28.35 1.2611 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

10a,b,c 74.8 69.3 69.3 69 73.6 83.9 52 0 0 28.86 1.2806 28.86 1.2806 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

11a,b,c 75.4 69.5 69.5 69.1 73.8 85.1 52 0 0 29.56 1.314 29.56 1.314 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

12a,b,c 75.6 69.6 69.6 69.3 74 85.4 52 0 0 30.26 1.343 30.26 1.343 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

13a,b,c 76.1 69.6 69.8 69.4 74.2 86.8 52 0 0 30.77 1.3632 30.77 1.3632 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

14a,b,c 76.5 69.9 69.9 69.8 74.3 87.8 52 0 0 31.65 1.4046 31.65 1.4046 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

15a,b,c 76.6 70.1 70.4 69.9 74.5 89.1 52 0 0 32.4 1.4332 32.4 1.4332 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

16a,b,c 77.2 70.5 70.6 70.1 74.6 89.4 52 0 0 33.12 1.4664 33.12 1.4664 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

17a,b,c 77.6 70.5 70.8 70.2 74.9 91.3 52 0 0 33.83 1.4937 33.83 1.4937 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

18a,b,c 78.5 70.7 71 70.4 75 92.1 52 0 0 34.83 1.5333 34.83 1.5333 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

19a,b,c 78.1 70.8 71.1 70.4 75.1 94 52 0 0 35.82 1.5811 35.82 1.5811 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

20a,b,c 79.2 71.1 71.3 70.7 75.3 94.8 52 0 0 36.97 1.624 36.97 1.624 water 0.563 0.521 0.559 0.546 0.342 0.407 0.027 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/27/2011 Remarks : Camera is focused on the last four crossover holes

26 psi not multiply by 2 yet not multiply by 2 yet

orange orange orange orange water orange water "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 62.6 65.6 65.9 65.6 70.8 74.7 44 0 0 26.14 0.5809 26.13 0.5783 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

2a,b,c 62.3 65.5 65.8 65.6 70.8 75.2 44 0 0 27.16 0.6024 27.18 0.6005 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

3a,b,c 62 65.5 65.7 65.4 70.9 75.9 44 0 0 28.14 0.6221 28.23 0.6225 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

4a,b,c 62.1 65.2 65.5 65.2 70.9 76.5 44 0 0 29.51 0.6508 29.26 0.6442 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

5a,b,c 61.5 65.2 65.4 65.2 70.9 77 44 0 0 30.35 0.6688 30.36 0.6674 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

6a,b,c 61.6 64.9 65.4 65 71.1 77.8 44 0 0 31.56 0.6943 31.49 0.6911 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

7a,b,c 61.1 64.8 65.1 64.9 71.1 78.7 44 0 0 32.61 0.7174 32.66 0.7158 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

8a,b,c 61.4 64.7 65.1 64.8 71 79.1 44 0 0 34 0.7468 33.75 0.7385 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

9a,b,c 61 64.6 65 64.6 71.1 80.4 44 0 0 34.79 0.761 34.86 0.7621 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

10a,b,c 60.5 64.3 64.7 64.4 70.9 81 44 0 0 35.97 0.7875 35.95 0.7849 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

11a,b,c 60.5 64.3 64.6 64.3 70.9 82.1 44 0 0 37.12 0.81 37.07 0.8081 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

12a,b,c 60.5 64.3 64.6 64.3 71 82.8 44 0 0 38.22 0.8335 38.22 0.8323 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

13a,b,c 60.5 64.2 64.5 64.3 71 83.8 44 0 0 39.32 0.8584 39.4 0.8566 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

14a,b,c 60.7 64.2 64.6 64.2 70.9 84.6 44 0 0 40.51 0.8823 40.62 0.8824 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

15a,b,c 60.3 64.1 64.5 64.1 70.9 86.1 44 0 0 41.65 0.9066 41.73 0.9058 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

16a,b,c 60.3 63.8 64.2 63.8 70.8 87.2 44 0 0 42.88 0.9318 43.04 0.9326 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

17a,b,c 60.3 63.9 64.2 63.8 70.9 89 44 0 0 44.13 0.9573 44.17 0.9558 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

18a,b,c 60.3 63.7 64.1 63.8 70.7 89.8 44 0 0 45.3 0.982 45.39 0.9809 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

19a,b,c 60.1 63.7 64 63.7 70.7 91.3 44 0 0 46.71 1.0107 46.67 1.0071 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

20a,b,c 59.9 63.5 63.9 63.6 70.7 92 44 0 0 47.82 1.0348 47.91 1.0328 orange/water 2.93 2.79 2.86 2.89 0.74 2.14 0.085 29.83

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -56

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/27/2011 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 69.2 66.8 67.2 66.8 69.9 74.3 41 0 0 27.15 0.6287 27.32 0.6318 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

2a,b,c 68 67 67.4 66.8 70.2 74.9 41 0 0 28.3 0.6558 28.33 0.6549 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

3a,b,c 68.7 67 67.3 66.8 70.3 75.4 41 0 0 29.61 0.6857 29.4 0.6799 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

4a,b,c 69.2 67.1 67.3 67 70.5 76.2 41 0 0 30.4 0.7039 30.64 0.7081 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

5a,b,c 69.3 67.1 67.4 67.1 70.6 76.9 41 0 0 31.57 0.7321 31.69 0.7324 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

6a,b,c 69.1 67.3 67.6 67 70.8 77.6 41 0 0 32.87 0.7614 32.95 0.7616 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

7a,b,c 69.6 67.1 67.4 67 71 78.2 41 0 0 34.12 0.7895 33.93 0.784 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

8a,b,c 69.8 67.1 67.4 67.1 70.9 79 41 0 0 35.19 0.8128 35.22 0.8128 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

9a,b,c 68.3 67.3 67.5 67.2 71.1 80.1 41 0 0 36.3 0.8391 36.36 0.8393 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

10a,b,c 69.9 67.1 67.4 67.1 71.1 81 41 0 0 37.37 0.8641 37.38 0.8626 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

11a,b,c 69.5 67.2 67.5 67.1 71.2 81.7 41 0 0 38.47 0.8898 38.42 0.8866 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

12a,b,c 69.2 67.4 67.7 67.3 71.4 82.5 41 0 0 39.52 0.9135 39.53 0.9117 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

13a,b,c 68.8 67.6 67.9 67.5 71.5 83.4 41 0 0 40.56 0.9376 40.75 0.9396 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

14a,b,c 70.7 67.8 67.9 67.7 71.6 84.3 41 0 0 41.89 0.9681 41.95 0.9671 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

15a,b,c 71.5 67.7 67.9 67.6 71.6 84.9 41 0 0 42.55 0.9826 42.5 0.9795 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

16a,b,c 70.5 67.9 68.1 67.8 71.8 85.6 41 0 0 43.2 0.9974 42.98 0.9903 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

17a,b,c 70.3 67.8 68 67.8 71.8 86.1 41 0 0 43.94 1.014 43.39 0.9996 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

18a,b,c 71.3 67.9 68.1 67.8 72 86.8 41 0 0 44.6 1.0296 43.95 1.0124 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

19a,b,c 71.2 68.1 68.3 68 72.1 87.4 41 0 0 45.14 1.042 44.45 1.0238 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

20a,b,c 71.4 68.2 68.5 68.1 72.2 87.9 41 0 0 45.59 1.052 44.99 1.036 orange 5.09 4.81 4.89 4.96 3.08 3.71 0.38 29.32

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/27/2011 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 72 63.9 64.4 64.1 67.3 72.7 39 0 0 29 0.6724 29.18 0.6745 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

2a,b,c 72.6 65.1 65.5 65.1 68.3 73.8 39 0 0 29.97 0.6946 30.25 0.6994 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

3a,b,c 73.4 66.2 66.6 66.1 69 74.7 39 0 0 31.47 0.728 31.37 0.7253 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

4a,b,c 73.7 66.9 67.2 66.8 69.5 75.7 39 0 0 32.61 0.7549 32.51 0.7514 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

5a,b,c 74.6 67.6 67.9 67.3 69.9 76.6 39 0 0 33.49 0.7752 33.56 0.7753 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

6a,b,c 73.9 68.2 68.5 67.9 70.4 77.5 39 0 0 34.58 0.8 34.64 0.8001 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

7a,b,c 74.7 68.7 68.9 68.4 70.7 78.3 39 0 0 35.65 0.8248 35.69 0.8244 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

8a,b,c 75.1 69.1 69.3 68.8 71 79.3 39 0 0 36.84 0.8522 36.79 0.8492 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

9a,b,c 75.3 69.4 69.6 69.1 71.4 80.1 39 0 0 38.11 0.8807 37.92 0.8753 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

10a,b,c 75.6 69.7 69.9 69.5 71.8 81.1 39 0 0 39.06 0.9034 38.94 0.8988 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

11a,b,c 75.5 70.1 70.2 69.7 72.1 82 39 0 0 40.15 0.928 40.11 0.9254 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

12a,b,c 76 70.1 70.3 69.8 72.2 82.8 39 0 0 41.12 0.9503 41.1 0.948 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

13a,b,c 75.9 70.3 70.4 70 72.4 83.6 39 0 0 42.26 0.9762 42.12 0.9714 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

14a,b,c 76.1 70.4 70.6 70.1 72.5 84.1 39 0 0 43.1 0.9957 43.02 0.9921 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

15a,b,c 75.6 70.6 70.7 70.3 72.8 84.7 39 0 0 43.9 1.013 43.8 1.0093 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

16a,b,c 75.5 70.8 70.9 70.6 73.1 85.6 39 0 0 44.34 1.0251 44.35 1.0223 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

17a,b,c 75.2 70.5 70.7 70.4 73 86 39 0 0 44.83 1.0352 44.94 1.0353 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

18a,b,c 75.1 70.6 70.8 70.5 73.1 86.4 39 0 0 45.44 1.0492 45.39 1.046 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

19a,b,c 75.1 70.4 70.6 70.4 73 86.9 39 0 0 46.12 1.0652 46.26 1.0657 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

20a,b,c 75.5 70.6 70.7 70.5 73.2 87.3 39 0 0 46.99 1.0864 47.03 1.083 orange 8.01 7.58 7.72 7.79 4.93 5.87 0.52 29.31

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -57

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/28/2011 Remarks : Camera is focused on the last four crossover holes

69 psi

DP, turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 68.9 64.4 64.8 64.3 67.1 72.1 37 0 0 31.34 0.7255 31.75 0.7337 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

2a,b,c 68.9 65.1 65.4 64.9 67.7 73.1 37 0 0 32.96 0.7637 33 0.7629 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

3a,b,c 69.2 65.6 66 65.4 68 73.7 37 0 0 34.02 0.7881 34.02 0.7865 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

4a,b,c 69.3 65.7 66.1 65.5 68.2 74.5 37 0 0 35.22 0.816 35.18 0.8129 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

5a,b,c 69.2 65.9 66.3 65.8 68.4 74.9 37 0 0 36.32 0.8407 36.22 0.8367 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

6a,b,c 69.4 66.2 66.5 66.1 68.5 75.5 37 0 0 37.47 0.8667 37.43 0.8643 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

7a,b,c 68.8 66.4 66.6 66.2 68.8 76.2 37 0 0 38.38 0.888 38.33 0.8853 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

8a,b,c 69.3 66.5 66.8 66.3 69.1 77 37 0 0 39.32 0.9097 39.42 0.91 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

9a,b,c 69.1 66.6 66.9 66.4 69.2 77.5 37 0 0 40.39 0.9341 40.4 0.9323 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

10a,b,c 68.9 66.7 66.9 66.6 69.3 78 37 0 0 41.52 0.9595 41.49 0.9574 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

11a,b,c 69.3 66.7 67 66.7 69.3 78.6 37 0 0 42.62 0.9854 42.57 0.9822 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

12a,b,c 68.7 66.8 67 66.7 69.4 79.3 37 0 0 43.68 1.0094 43.62 1.006 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

13a,b,c 69.1 66.9 67.1 66.7 69.6 80 37 0 0 44.4 1.0258 44.51 1.0266 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

14a,b,c 68.5 66.8 67 66.6 69.6 80.6 37 0 0 45.72 1.0553 45.6 1.0512 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

15a,b,c 69.1 66.9 67.1 66.8 69.7 81.2 37 0 0 46.68 1.0777 46.58 1.0733 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

16a,b,c 69.1 66.9 67.2 66.8 69.8 81.8 37 0 0 47.74 1.1029 47.65 1.0979 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

17a,b,c 68.2 66.8 67.1 66.7 69.8 82.4 37 0 0 48.59 1.1221 48.58 1.1193 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

18a,b,c 68.4 66.8 67 66.6 69.8 82.9 37 0 0 49.82 1.1496 49.74 1.1454 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

19a,b,c 68.3 66.8 67 66.7 69.8 83.8 37 0 0 50.97 1.1761 51 1.1734 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

20a,b,c 68.6 66.8 67 66.7 69.9 84.4 37 0 0 52.24 1.2043 52.26 1.2024 orange 11.91 11.32 11.57 11.6 7.29 8.75 0.84 29.31

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/28/2011 Remarks : Camera is focused on the last four cross-over holes

80 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.7 65 65.2 65 66.8 71.9 36 0 0 32.48 0.7525 32.41 0.7485 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

2a,b,c 71.8 65.8 66 65.7 67.8 73 36 0 0 33.46 0.7761 33.55 0.7757 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

3a,b,c 71.6 66.4 66.6 66.3 68.2 73.8 36 0 0 34.72 0.8046 34.77 0.8036 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

4a,b,c 72.1 66.7 67 66.5 68.7 74.6 36 0 0 35.83 0.8303 35.88 0.829 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

5a,b,c 71.6 67.1 67.3 66.9 69 75.2 36 0 0 36.97 0.8556 36.95 0.8538 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

6a,b,c 71.4 67.3 67.5 67.1 69.3 76 36 0 0 38.14 0.8826 38.07 0.8794 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

7a,b,c 71.9 67.4 67.6 67.2 69.4 76.4 36 0 0 39.12 0.9051 39.13 0.9035 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

8a,b,c 71.5 67.4 67.6 67.2 69.5 77.2 36 0 0 40.26 0.9312 40.25 0.9291 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

9a,b,c 70.4 67.4 67.6 67.2 69.6 77.6 36 0 0 41.42 0.9579 41.39 0.9554 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

10a,b,c 70.9 67.5 67.7 67.3 69.8 78.2 36 0 0 42.44 0.9808 42.43 0.9792 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

11a,b,c 70.5 67.5 67.8 67.4 69.9 78.8 36 0 0 43.67 1.0092 43.67 1.0075 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

12a,b,c 70.6 67.5 67.7 67.4 69.9 79.4 36 0 0 44.94 1.0382 44.99 1.0377 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

13a,b,c 70.3 67.5 67.7 67.3 70 80.1 36 0 0 46.17 1.0667 46.21 1.0656 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

14a,b,c 70.5 67.5 67.8 67.4 70.1 80.8 36 0 0 47.42 1.0958 47.42 1.0932 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

15a,b,c 70.7 67.4 67.6 67.3 70 81.1 36 0 0 48.62 1.1221 48.64 1.1209 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

16a,b,c 71.1 67.5 67.7 67.4 70.1 82.5 36 0 0 49.84 1.1506 49.87 1.1484 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

17a,b,c 71.5 67.7 68 67.6 70.2 83 36 0 0 51.02 1.1773 51.07 1.176 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

18a,b,c 71 67.9 68.1 67.8 70.4 84.4 36 0 0 52.6 1.2136 52.38 1.2058 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

19a,b,c 71.6 68.1 68.4 68 70.6 85.1 36 0 0 54.12 1.2481 53.58 1.233 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

20a,b,c 71.1 68.2 68.4 68.1 70.7 86.2 36 0 0 56.09 1.2928 55.05 1.2663 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -58

11crossover holes-9 exit holes, staggered arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:02/11/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 71.0 70.8 71.0 70.8 71.5 80.8 71.6 0 0 21.60 0.5009 20.14 0.4660 water 0.751 0.714 0.73 0.734 0.495 0.609 0.041 29.97

2a,b,c 71.0 71.0 71.2 70.9 71.7 81.3 71.6 0 0 22.25 0.5161 21.04 0.4869 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

3a,b,c 71.1 71.1 71.2 71.0 71.7 82.0 71.6 0 0 22.56 0.5234 21.84 0.5054 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

4a,b,c 70.9 71.1 71.2 71.0 71.7 82.9 71.6 0 0 23.01 0.5337 22.57 0.5220 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

5a,b,c 71.0 71.0 71.2 70.9 71.7 83.6 71.6 0 0 23.44 0.5436 23.37 0.5404 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

6a,b,c 71.1 71.0 71.2 71.0 71.8 84.4 71.6 0 0 24.21 0.5614 24.23 0.5601 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

7a,b,c 71.3 71.1 71.2 71.0 71.8 85.2 71.6 0 0 25.11 0.5823 25.06 0.5792 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

8a,b,c 71.2 71.1 71.2 71.0 71.8 86.6 71.6 0 0 25.84 0.5991 25.94 0.5995 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

9a,b,c 71.2 71.1 71.3 71.0 71.9 87.7 71.6 0 0 26.70 0.6190 26.77 0.6184 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

10a,b,c 71.0 71.2 71.4 71.0 71.9 88.5 71.6 0 0 27.48 0.6369 27.50 0.6352 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

11a,b,c 71.3 71.1 71.2 71.0 71.9 90.0 71.4 0 0 28.33 0.6564 28.35 0.6546 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

12a,b,c 71.2 71.0 71.2 70.9 71.9 90.8 71.4 0 0 29.12 0.6748 29.16 0.6733 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

13a,b,c 71.2 71.0 71.3 71.0 71.9 92.4 71.4 0 0 29.91 0.6928 29.94 0.6913 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

14a,b,c 70.9 71.0 71.2 70.9 72.0 93.2 71.4 0 0 30.54 0.7072 30.57 0.7054 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

15a,b,c 71.2 71.1 71.3 71.0 72.0 94.2 71.4 0 0 31.08 0.7197 31.04 0.7163 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

16a,b,c 71.4 71.1 71.3 71.1 72.0 95.0 71.4 0 0 31.78 0.7359 31.85 0.7348 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

17a,b,c 71.6 71.1 71.3 71.1 72.0 96.4 71.4 0 0 32.68 0.7566 32.75 0.7551 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

18a,b,c 71.2 71.1 71.3 71.0 72.1 97.7 71.4 0 0 33.62 0.7780 33.57 0.7741 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

19a,b,c 71.4 71.1 71.3 71.0 72.1 99.0 71.4 0 0 34.45 0.7972 34.36 0.7921 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

20a,b,c 71.0 71.0 71.2 70.9 72.1 100.2 71.4 0 0 35.15 0.8134 35.05 0.8018 water 0.751 0.714 0.73 0.734 0.495 0.609 0.027 29.97

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:02/11/2012 Remarks : Camera is focused on the last four crossover holes

26 psi

"Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 77.1 74.7 74.8 74.4 74.5 79.4 75.1 0 0 21.63 0.5017 21.15 0.4894 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

2a,b,c 78.2 75.2 75.3 74.9 75.0 80.8 75.1 0 0 21.99 0.5101 21.97 0.5082 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

3a,b,c 78.0 75.4 75.4 75.0 75.2 81.6 75.1 0 0 22.71 0.5268 22.55 0.5213 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

4a,b,c 77.2 75.5 75.5 75.1 75.3 82.0 75.1 0 0 22.98 0.5331 23.06 0.5332 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

5a,b,c 77.3 75.5 75.6 75.2 75.5 82.7 75.1 0 0 23.65 0.5484 23.57 0.5449 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

6a,b,c 77.6 75.7 75.8 75.4 75.6 83.3 75.1 0 0 24.13 0.5594 24.21 0.5596 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

7a,b,c 78.1 75.7 75.8 75.4 75.6 83.8 75.1 0 0 24.79 0.5746 24.92 0.5755 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

8a,b,c 78.3 75.8 75.9 75.5 75.7 84.8 75.1 0 0 25.48 0.5907 25.65 0.5929 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

9a,b,c 78.1 75.9 76.0 75.6 75.9 85.5 75.1 0 0 26.06 0.6042 26.15 0.6045 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

10a,b,c 78.5 75.9 76.1 75.6 75.9 85.9 75.1 0 0 26.79 0.6208 26.92 0.6219 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

11a,b,c 78.6 76.1 76.1 75.8 75.9 86.6 75.1 0 0 27.56 0.6387 27.54 0.6358 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

12a,b,c 78.6 76.0 76.2 75.7 76.0 86.7 75.1 0 0 28.28 0.6551 28.36 0.6549 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

13a,b,c 79.2 76.0 76.1 75.8 75.9 88.0 75.1 0 0 28.93 0.6706 28.84 0.6662 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

14a,b,c 78.9 76.1 76.2 75.9 76.0 88.2 75.1 0 0 29.40 0.6812 29.43 0.6797 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

15a,b,c 79.2 76.1 76.2 75.8 76.0 89.0 75.1 0 0 30.13 0.6977 30.09 0.6947 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

16a,b,c 79.3 76.3 76.3 76.0 76.0 89.6 75.1 0 0 30.76 0.7124 30.61 0.7068 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

17a,b,c 78.4 76.2 76.3 76.0 76.1 90.3 75.1 0 0 31.35 0.7261 31.45 0.7253 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

18a,b,c 79.1 76.4 76.5 76.2 76.2 91.2 75.1 0 0 32.40 0.7501 32.30 0.7450 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

19a,b,c 78.3 76.4 76.5 76.1 76.3 92.4 75.1 0 0 33.44 0.7735 33.34 0.7689 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

20a,b,c 79.2 76.6 76.6 76.3 76.3 93.6 75.1 0 0 34.48 0.7970 34.51 0.7963 orange 3.390 3.180 3.270 3.280 2.150 2.710 0.210 30.34

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -59

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:02/11/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.5 74.7 74.9 74.7 75.4 79.4 74.2 0 0 22.29 0.5170 22.37 0.5176 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

2a,b,c 76.8 74.9 75.0 74.9 75.4 80.1 74.2 0 0 23.17 0.5374 23.22 0.5368 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

3a,b,c 76.6 75.0 75.1 74.9 75.5 80.6 74.2 0 0 24.02 0.5573 24.04 0.5559 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

4a,b,c 76.8 75.1 75.3 75.1 75.5 81.2 74.2 0 0 24.86 0.5765 24.83 0.5738 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

5a,b,c 76.7 75.3 75.4 75.2 75.7 81.6 74.2 0 0 25.65 0.5946 25.70 0.5941 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

6a,b,c 76.3 75.2 75.3 75.1 75.6 82.2 74.2 0 0 26.50 0.6143 26.43 0.6109 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

7a,b,c 75.8 75.2 75.3 75.1 75.7 82.6 74.2 0 0 27.23 0.6316 27.31 0.6313 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

8a,b,c 76.1 75.0 75.1 74.9 75.6 82.8 74.2 0 0 28.09 0.6512 28.08 0.6491 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

9a,b,c 75.8 74.8 74.9 74.8 75.4 83.2 74.2 0 0 28.80 0.6676 28.83 0.6661 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

10a,b,c 75.8 74.7 74.8 74.6 75.3 83.7 74.2 0 0 29.59 0.6856 29.69 0.6857 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

11a,b,c 75.6 74.6 74.8 74.6 75.4 84.5 74.2 0 0 30.48 0.7062 30.51 0.7046 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

12a,b,c 75.0 74.5 74.6 74.5 75.3 84.4 74.2 0 0 31.27 0.7242 31.39 0.7248 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

13a,b,c 75.3 74.2 74.5 74.3 75.1 85.0 74.2 0 0 32.07 0.7430 32.31 0.7460 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

14a,b,c 75.3 74.2 74.4 74.2 75.0 85.5 74.2 0 0 33.15 0.7676 33.21 0.7664 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

15a,b,c 74.6 74.1 74.4 74.2 75.0 86.4 74.2 0 0 34.10 0.7891 34.00 0.7850 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

16a,b,c 74.4 74.2 74.4 74.2 75.0 86.9 74.2 0 0 34.88 0.8074 34.96 0.8067 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

17a,b,c 74.6 74.2 74.3 74.2 75.0 87.2 74.2 0 0 35.73 0.8268 35.75 0.8249 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

18a,b,c 74.3 74.1 74.3 74.2 74.9 87.9 74.2 0 0 36.60 0.8470 36.59 0.8442 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

19a,b,c 75.2 74.1 74.2 74.1 74.9 88.6 74.2 0 0 37.64 0.8707 37.70 0.8697 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

20a,b,c 74.6 74.1 74.2 74.1 74.9 89.6 74.2 0 0 38.81 0.8976 38.70 0.8931 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

21a,b,c 74.7 74.1 74.2 74.1 74.9 90.6 74.2 0 0 40.00 0.9251 39.96 0.9212 orange 5.880 5.590 5.710 5.740 3.770 4.680 0.350 30.33

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:02/21/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.3 74.9 75 74.8 75.3 79.5 71.9 0 0 23.13 0.5363 22.6 0.5226 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

2a,b,c 75.5 74.7 74.9 74.7 75.3 79.6 71.9 0 0 23.51 0.5456 23.63 0.5463 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

3a,b,c 75.9 74.4 74.6 74.4 75 79.8 71.9 0 0 24.67 0.5722 24.79 0.5736 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

4a,b,c 75.8 74.3 74.5 74.3 75 80.1 71.9 0 0 25.71 0.5962 25.66 0.5932 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

5a,b,c 75 74.3 74.5 74.3 74.9 80.5 71.9 0 0 26.81 0.6215 26.94 0.6228 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

6a,b,c 76.2 74.3 74.5 74.4 74.9 81 71.9 0 0 27.96 0.6483 28.1 0.6496 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

7a,b,c 76 74.4 74.5 74.4 74.9 81.9 71.9 0 0 29.17 0.676 29.16 0.6741 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

8a,b,c 75.4 74.4 74.6 74.4 75 82 71.9 0 0 30.31 0.7025 30.43 0.7029 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

9a,b,c 76.1 74.4 74.6 74.4 74.9 82.8 71.9 0 0 31.57 0.7313 31.46 0.727 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

10a,b,c 75.8 74.4 74.6 74.4 75 83.3 71.9 0 0 32.61 0.7553 32.61 0.7531 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

11a,b,c 75.6 74.4 74.6 74.4 75 84 71.9 0 0 33.81 0.7833 33.72 0.7788 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

12a,b,c 75.6 74.4 74.5 74.4 75 84.6 71.9 0 0 34.89 0.8076 34.85 0.8044 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

13a,b,c 74.7 74.3 74.4 74.3 74.9 84.9 71.9 0 0 35.92 0.8312 35.99 0.8306 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

14a,b,c 75.2 74.2 74.3 74.2 74.9 85.5 71.9 0 0 37.11 0.8588 37.11 0.8562 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

15a,b,c 75.2 74 74.2 74 74.8 86 71.9 0 0 38.19 0.8833 38.17 0.8806 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

16a,b,c 75.2 73.8 73.9 73.8 74.7 86.8 71.9 0 0 39.35 0.9103 39.34 0.9076 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

17a,b,c 74.4 73.7 73.9 73.8 74.7 87.4 71.9 0 0 40.4 0.9342 40.46 0.9329 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

18a,b,c 75.1 73.6 73.8 73.7 74.5 88 71.9 0 0 41.67 0.9633 41.56 0.9583 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

19a,b,c 75.3 73.6 73.7 73.6 74.5 89.1 71.9 0 0 42.83 0.9901 42.8 0.9863 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

20a,b,c 74.6 73.5 73.6 73.5 74.4 90 71.9 0 0 43.99 1.0163 43.97 1.0128 orange 9.06 8.64 8.79 8.84 5.69 7.24 0.59 30.3

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -60

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:02/21/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP, turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.6 73.9 74 73.8 74.3 78.6 71 0 0 25.91 0.602 25.71 0.5948 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

2a,b,c 76.2 74 74.1 73.9 74.3 79 71 0 0 27.01 0.6263 26.98 0.6238 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

3a,b,c 76.5 74 74.1 73.9 74.3 79.6 71 0 0 28.11 0.6516 28.05 0.6486 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

4a,b,c 76.3 74 74.1 73.9 74.3 80.1 71 0 0 29.29 0.6789 29.21 0.6754 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

5a,b,c 75.7 74 74.1 73.9 74.4 80.6 71 0 0 30.33 0.7031 30.36 0.7017 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

6a,b,c 75.7 73.9 74.1 73.9 74.3 80.9 71 0 0 31.41 0.7278 31.45 0.727 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

7a,b,c 75.7 73.9 73.9 73.8 74.3 81.2 71 0 0 32.69 0.7574 32.58 0.7527 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

8a,b,c 75.6 73.6 73.8 73.6 74.2 81.9 71 0 0 33.7 0.7805 33.69 0.7781 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

9a,b,c 75.6 73.7 73.9 73.7 74.3 82.5 71 0 0 34.83 0.806 34.92 0.8061 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

10a,b,c 76.3 73.9 74 73.8 74.3 83.2 71 0 0 36.05 0.8345 36 0.8314 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

11a,b,c 76.3 74 74.1 73.9 74.4 83.9 71 0 0 37.16 0.8602 37.06 0.8555 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

12a,b,c 76.4 74 74.2 74 74.5 84.5 71 0 0 38.28 0.8856 38.16 0.8805 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

13a,b,c 76.3 74.1 74.2 74 74.6 85.1 71 0 0 39.42 0.9126 39.39 0.9091 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

14a,b,c 76 74.1 74.2 74 74.6 85.9 71 0 0 40.57 0.9384 40.94 0.9436 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

15a,b,c 75.9 73.9 74.1 73.9 74.6 86.8 71 0 0 42.03 0.972 42.06 0.9699 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

16a,b,c 75.2 73.8 73.9 73.7 74.5 87.3 71 0 0 43.17 0.9981 43.2 0.9959 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

17a,b,c 75.1 73.6 73.7 73.5 74.4 88 71 0 0 44.43 1.0263 44.34 1.0221 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

18a,b,c 74.7 73.4 73.6 73.4 74.3 88.8 71 0 0 45.41 1.049 45.38 1.0454 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

19a,b,c 75.1 73.3 73.4 73.3 74.2 89.1 71 0 0 46.52 1.0758 46.54 1.0709 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

20a,b,c 74.7 73.1 73.2 73.1 74.1 89.5 71 0 0 47.94 1.1064 47.93 1.103 orange 13.26 12.63 12.9 12.98 8.5 10.61 0.81 30.26

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross9exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:02/21/2011 Remarks : Camera is focused on the last four cross-over holes

80 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.5 74.2 74.4 74.1 74.4 78.5 70.7 0 0 26.48 0.6141 26.24 0.6071 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

2a,b,c 77.8 74.5 74.6 74.4 74.6 79.2 70.7 0 0 27.42 0.6358 27.41 0.6336 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

3a,b,c 76.7 74.6 74.7 74.4 74.7 79.9 70.7 0 0 28.55 0.6614 28.63 0.6616 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

4a,b,c 76.6 74.7 74.8 74.6 74.9 80.4 70.7 0 0 29.71 0.6884 29.72 0.6871 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

5a,b,c 77 74.6 74.7 74.5 74.9 8.08 70.7 0 0 30.82 0.7142 30.83 0.7125 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

6a,b,c 76.7 74.5 74.7 74.5 74.9 81.3 70.7 0 0 32.04 0.7424 32.08 0.7413 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

7a,b,c 76.3 74.3 74.4 74.2 74.8 81.7 70.7 0 0 33.3 0.7719 33.33 0.7703 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

8a,b,c 75.9 73.9 74.1 73.9 74.6 82.1 70.7 0 0 34.54 0.7998 34.68 0.801 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

9a,b,c 75.8 73.8 73.9 73.7 74.5 82.5 70.7 0 0 35.89 0.8305 35.87 0.8287 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

10a,b,c 76 73.7 73.8 73.6 74.4 82.9 70.7 0 0 37.09 0.8588 37.03 0.8544 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

11a,b,c 75.1 73.5 73.6 73.5 74.2 83.3 70.7 0 0 38.3 0.886 38.3 0.884 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

12a,b,c 75.3 73.5 73.7 73.5 74.2 84 70.7 0 0 39.55 0.9155 39.52 0.9121 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

13a,b,c 75.4 73.6 73.8 73.6 74.3 84.9 70.7 0 0 40.85 0.9452 40.77 0.941 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

14a,b,c 76.5 73.6 73.8 73.5 74.2 85.4 70.7 0 0 41.99 0.971 42.04 0.9698 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

15a,b,c 76.4 73.7 73.8 73.6 74.2 86.2 70.7 0 0 43.42 1.0041 43.39 1.0009 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

16a,b,c 76.3 73.6 73.7 73.6 74.1 86.8 70.7 0 0 44.65 1.0324 44.54 1.0266 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

17a,b,c 75.2 73.6 73.7 73.5 74.2 87.5 70.7 0 0 45.82 1.0583 45.88 1.0567 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

18a,b,c 74.9 73.3 73.5 73.3 74.1 88.2 70.7 0 0 47.13 1.0891 47.19 1.0865 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

19a,b,c 75.7 73.3 73.5 73.3 74.1 88.9 70.7 0 0 48.29 1.1155 48.46 1.1161 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

20a,b,c 74.5 73.1 73.2 73.1 73.9 89.8 70.7 0 0 49.98 1.1547 49.93 1.1499 orange 17.1 16.32 16.67 16.78 10.89 13.57 1.08 30.21

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -61

11crossover holes-8 exit holes, staggered arrangement, 5 degree tilt angle, no bleed

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross8exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2. not multiply by 2 yet

Date:3/05/2012 Remarks : Camera is focused on the last four crossover holes

13 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.2 74.3 74.4 74.1 74.8 80.6 74.2 0 0 18.66 0.4328 18.54 0.4285 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

2a,b,c 74.5 74.2 74.4 74.0 74.8 81.6 74.2 0 0 19.28 0.4471 19.09 0.4414 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

3a,b,c 74.2 74.1 74.3 74.1 74.8 82.6 74.2 0 0 19.86 0.4608 19.95 0.4613 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

4a,b,c 74.4 74.1 74.2 74.0 74.7 83.3 74.2 0 0 20.44 0.4740 20.54 0.4750 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

5a,b,c 73.8 74.0 74.2 73.9 74.7 84.1 74.2 0 0 21.07 0.4889 21.00 0.4856 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

6a,b,c 74.3 74.0 74.2 74.0 74.7 84.6 74.2 0 0 21.60 0.5010 21.47 0.4962 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

7a,b,c 74.3 74.0 74.2 74.0 74.7 85.3 74.2 0 0 22.02 0.5109 22.05 0.5096 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

8a,b,c 73.8 74.1 74.3 74.0 74.7 86.1 74.2 0 0 22.59 0.5239 22.58 0.5217 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

9a,b,c 74.0 74.2 74.4 74.1 74.8 87.1 74.2 0 0 23.02 0.5337 23.05 0.5320 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

10a,b,c 73.9 74.1 74.4 74.0 74.9 87.8 74.2 0 0 23.56 0.5463 23.57 0.5446 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

11a,b,c 73.8 74.2 74.4 74.1 74.9 88.6 74.2 0 0 24.03 0.5573 24.13 0.5576 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

12a,b,c 74.2 74.3 74.5 74.3 74.9 89.4 74.2 0 0 24.67 0.5719 24.57 0.5674 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

13a,b,c 73.8 74.3 74.5 74.2 75.0 90.2 74.2 0 0 25.03 0.5801 25.15 0.5810 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

14a,b,c 74.3 74.3 74.4 74.2 75.0 90.6 74.2 0 0 25.59 0.5930 25.60 0.5914 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

15a,b,c 73.6 74.1 74.3 74.0 75.0 91.3 74.2 0 0 26.18 0.6068 26.09 0.6022 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

16a,b,c 73.9 74.2 74.3 74.1 75.0 92.1 74.2 0 0 26.56 0.6155 26.61 0.6142 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

17a,b,c 73.7 74.0 74.2 74.0 74.9 92.9 74.2 0 0 27.06 0.6272 27.08 0.6250 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

18a,b,c 73.8 73.9 74.2 73.9 74.9 93.2 74.2 0 0 27.84 0.6450 27.75 0.6404 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

19a,b,c 73.2 73.8 74.0 73.8 74.9 94.1 74.2 0 0 28.49 0.6601 28.36 0.6546 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

20a,b,c 73.6 73.7 73.9 73.7 74.7 95.4 74.2 0 0 29.15 0.6752 29.08 0.6708 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

21a,b,c 72.9 73.6 73.8 73.6 74.7 96.4 74.2 0 0 30.04 0.6956 30.00 0.6919 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

22a,b,c 73.1 73.6 73.9 73.6 74.7 97.4 74.2 0 0 31.01 0.7176 31.15 0.7187 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

23a,b,c 73.6 73.7 73.9 73.7 74.7 99.3 74.2 0 0 32.12 0.7436 32.09 0.7400 water 0.834 0.800 0.807 0.814 0.569 0.712 0.042 29.98

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross8exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/05/2012 Remarks : Camera is focused on the last four crossover holes

26 psi not multiply by 2 yet not multiply by 2 yet

orange orange orange orange water orange water "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 74.8 74.6 74.8 74.5 75.4 80.6 21.12 0 0 21.12 0.4900 20.99 0.4852 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

2a,b,c 74.1 74.5 74.7 74.4 75.4 81.6 21.81 0 0 21.81 0.5060 21.76 0.5033 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

3a,b,c 74.4 74.4 74.6 74.3 75.3 82.3 22.50 0 0 22.50 0.5221 22.44 0.5190 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

4a,b,c 74.2 74.3 74.5 74.2 75.2 82.8 23.23 0 0 23.23 0.5388 23.19 0.5362 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

5a,b,c 74.7 74.2 74.4 74.1 75.1 83.7 24.01 0 0 24.01 0.5569 24.08 0.5565 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

6a,b,c 74.7 74.1 74.3 74.0 75.0 84.3 24.88 0 0 24.88 0.5769 24.88 0.5748 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

7a,b,c 74.0 74.0 74.2 73.9 74.9 85.0 25.63 0 0 25.63 0.5944 25.68 0.5934 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

8a,b,c 74.8 74.0 74.2 73.9 74.9 85.6 26.23 0 0 26.23 0.6080 26.26 0.6069 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

9a,b,c 73.8 73.8 74.0 73.7 74.7 86.0 27.02 0 0 27.02 0.6263 27.07 0.6253 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

10a,b,c 73.6 73.8 74.0 73.7 74.7 86.9 27.79 0 0 27.79 0.6443 27.89 0.6445 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

11a,b,c 74.3 73.8 74.0 73.7 74.7 87.6 28.78 0 0 28.78 0.6670 28.63 0.6612 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

12a,b,c 73.4 73.7 73.9 73.6 74.6 88.4 29.46 0 0 29.46 0.6829 29.53 0.6818 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

13a,b,c 73.6 73.7 73.9 73.6 74.6 89.2 30.06 0 0 30.06 0.6968 30.15 0.6959 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

14a,b,c 73.4 73.7 73.9 73.6 74.6 90.1 30.90 0 0 30.90 0.7157 30.95 0.7144 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

15a,b,c 73.6 73.9 74.1 73.8 74.8 91.1 31.82 0 0 31.82 0.7370 31.71 0.7319 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

16a,b,c 74.6 73.9 74.1 73.8 74.8 92.3 32.57 0 0 32.57 0.7542 32.51 0.7499 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

17a,b,c 73.8 73.9 74.1 73.8 74.8 93.4 33.40 0 0 33.40 0.7733 33.41 0.7700 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

18a,b,c 74.1 74.1 74.3 74.0 75.0 94.6 34.39 0 0 34.39 0.7959 34.41 0.7935 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

19a,b,c 74.1 74.0 74.2 73.9 75.0 95.9 35.26 0 0 35.26 0.8158 35.25 0.8125 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

20a,b,c 74.5 74.0 74.2 73.9 75.0 96.9 36.18 0 0 36.18 0.8373 36.18 0.8338 orange/water 4.080 3.910 3.940 3.980 2.770 3.450 0.200 30.04

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -62

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross8exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/05/2012 Remarks : Camera is focused on the last four crossover holes

40 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 76.0 73.9 74.0 73.7 74.3 78.7 70.2 0 0 21.56 0.5002 21.59 0.4995 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

2a,b,c 75.7 74.1 74.2 73.9 74.5 79.6 70.2 0 0 22.47 0.5215 22.45 0.5191 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

3a,b,c 75.5 74.2 74.3 74.1 74.5 80.1 70.2 0 0 23.25 0.5393 23.31 0.5388 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

4a,b,c 75.9 74.1 74.3 74.0 74.6 80.8 70.2 0 0 24.09 0.5589 24.05 0.5559 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

5a,b,c 75.1 74.0 74.2 73.9 74.5 81.4 70.2 0 0 24.97 0.5790 24.94 0.5765 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

6a,b,c 74.3 73.8 74.0 73.8 74.4 81.7 70.2 0 0 25.73 0.5965 25.65 0.5930 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

7a,b,c 74.7 73.6 73.9 73.6 74.3 82.4 70.2 0 0 26.51 0.6146 26.56 0.6138 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

8a,b,c 74.4 73.5 73.8 73.4 74.3 83.0 70.2 0 0 27.50 0.6376 27.52 0.6362 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

9a,b,c 74.3 73.6 73.7 73.5 74.3 83.4 70.2 0 0 28.39 0.6582 28.46 0.6575 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

10a,b,c 73.7 73.4 73.6 73.4 74.2 83.9 70.2 0 0 29.29 0.6787 29.36 0.6781 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

11a,b,c 73.1 73.2 73.4 73.2 74.1 84.5 70.2 0 0 30.24 0.7006 30.34 0.7006 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

12a,b,c 72.9 73.3 73.5 73.3 74.1 85.1 70.2 0 0 31.23 0.7235 31.26 0.7217 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

13a,b,c 73.1 73.2 73.4 73.1 74.1 85.8 70.2 0 0 32.39 0.7505 32.42 0.7484 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

14a,b,c 73.0 73.3 73.4 73.3 74.2 86.6 70.2 0 0 33.33 0.7721 33.30 0.7686 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

15a,b,c 73.5 73.1 73.3 73.1 74.2 87.7 70.2 0 0 34.28 0.7938 34.25 0.7900 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

16a,b,c 72.9 73.2 73.3 73.2 74.2 88.0 70.2 0 0 35.21 0.8151 35.25 0.8130 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

17a,b,c 72.9 73.2 73.4 73.2 74.2 89.0 70.2 0 0 36.12 0.8355 36.18 0.8347 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

18a,b,c 73.6 73.1 73.2 73.0 74.1 90.2 70.2 0 0 37.32 0.8636 37.30 0.8600 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

19a,b,c 73.2 73.0 73.2 73.0 74.1 91.0 70.2 0 0 38.34 0.8871 38.38 0.8847 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

20a,b,c 73.7 72.8 73.1 72.8 74.1 92.0 70.2 0 0 39.49 0.9130 39.34 0.9066 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

21a,b,c 72.8 72.8 73.0 72.7 74.0 92.8 70.2 0 0 40.41 0.9342 40.37 0.9303 orange 7.220 6.970 7.090 7.110 4.930 6.190 0.390 30.05

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross8exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/05/2012 Remarks : Camera is focused on the last four crossover holes

54 psi

DP,turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.3 73.3 73.4 73.2 73.6 78.1 74.2 0 0 23.03 0.5343 23.04 0.5328 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

2a,b,c 75.6 73.5 73.6 73.4 73.8 78.7 74.2 0 0 24.02 0.5572 24.08 0.5570 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

3a,b,c 75.1 73.7 73.8 73.6 73.9 79.6 74.2 0 0 25.03 0.5807 25.05 0.5793 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

4a,b,c 74.8 73.8 73.9 73.6 74.0 80.3 74.2 0 0 26.11 0.6054 26.03 0.6018 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

5a,b,c 74.1 73.8 73.9 73.7 74.1 80.7 74.2 0 0 27.05 0.6272 27.03 0.6249 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

6a,b,c 74.7 73.6 73.8 73.6 74.2 81.4 74.2 0 0 28.05 0.6501 28.03 0.6480 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

7a,b,c 74.0 73.3 73.5 73.3 74.0 81.9 74.2 0 0 29.21 0.6771 29.09 0.6722 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

8a,b,c 73.7 73.1 73.3 73.0 74.0 82.4 74.2 0 0 30.20 0.6999 30.19 0.6974 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

9a,b,c 73.3 72.9 73.1 72.7 73.8 82.9 74.2 0 0 31.12 0.7212 31.01 0.7163 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

10a,b,c 73.2 72.5 72.7 72.4 73.5 83.3 74.2 0 0 32.14 0.7448 32.15 0.7425 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

11a,b,c 73.4 72.4 72.6 72.4 73.5 83.8 74.2 0 0 32.99 0.7642 33.14 0.7652 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

12a,b,c 73.1 72.3 72.6 72.2 73.4 84.7 74.2 0 0 34.50 0.7991 34.52 0.7968 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

13a,b,c 73.6 72.2 72.5 72.2 73.3 85.4 74.2 0 0 35.81 0.8291 35.90 0.8286 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

14a,b,c 73.6 72.3 72.5 72.3 73.3 86.4 74.2 0 0 37.31 0.8637 37.28 0.8597 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

15a,b,c 73.9 72.3 72.5 72.2 73.2 87.5 74.2 0 0 38.64 0.8943 38.67 0.8916 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

16a,b,c 74.1 72.4 72.6 72.3 73.3 88.5 74.2 0 0 40.08 0.9269 40.21 0.9268 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

17a,b,c 73.6 72.5 72.7 72.5 73.4 89.7 74.2 0 0 41.51 0.9603 41.44 0.9551 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

18a,b,c 73.3 72.6 72.8 72.6 73.5 90.7 74.2 0 0 42.07 0.9729 42.16 0.9715 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

19a,b,c 73.5 72.7 72.9 72.6 73.6 81.5 74.2 0 0 43.05 0.9952 43.14 0.9936 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

20a,b,c 73.5 72.8 73.0 72.7 73.7 92.3 74.2 0 0 44.09 1.0185 44.16 1.0162 orange 11.200 10.790 10.960 11.020 7.660 9.580 0.690 30.03

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

A -63

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross8exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:3/05/2012 Remarks : Camera is focused on the last four crossover holes

69 psi

DP, turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 75.0 71.4 71.4 71.2 71.1 75.8 69.3 0 0 26.00 0.6032 26.18 0.6055 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

2a,b,c 75.1 71.6 71.7 71.5 71.4 76.6 69.3 0 0 27.23 0.6317 27.23 0.6296 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

3a,b,c 75.5 71.8 71.9 71.6 71.6 77.4 69.3 0 0 28.22 0.6544 28.30 0.6544 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

4a,b,c 75.7 72.1 72.2 71.9 71.8 78.1 69.3 0 0 29.42 0.6818 29.38 0.6792 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

5a,b,c 75.2 72.4 72.4 72.2 72.1 78.9 69.3 0 0 30.52 0.7076 30.51 0.7052 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

6a,b,c 76.2 72.6 72.7 72.4 72.3 79.6 69.3 0 0 31.42 0.7281 31.58 0.7296 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

7a,b,c 76.8 72.9 72.9 72.6 72.6 80.3 69.3 0 0 32.32 0.7490 32.22 0.7443 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

8a,b,c 76.6 73.1 73.2 72.9 72.9 81.1 69.3 0 0 33.26 0.7707 33.09 0.7634 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

9a,b,c 76.9 73.5 73.6 73.2 73.1 82.0 69.3 0 0 34.28 0.7940 34.08 0.7872 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

10a,b,c 78.2 73.8 73.9 73.6 73.4 82.7 69.3 0 0 35.01 0.8108 35.18 0.8123 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

11a,b,c 78.2 74.1 74.2 73.9 73.7 83.5 68.9 0 0 36.11 0.8364 36.24 0.8367 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

12a,b,c 78.7 74.4 74.5 74.1 73.9 84.5 68.9 0 0 37.34 0.8647 37.49 0.8651 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

13a,b,c 79.2 74.7 74.7 74.5 74.1 85.3 68.9 0 0 38.64 0.8943 38.53 0.8889 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

14a,b,c 79.7 74.9 75.0 74.7 74.4 86.4 68.9 0 0 39.61 0.9166 39.71 0.9159 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

15a,b,c 79.5 75.0 75.1 74.7 74.5 87.1 68.9 0 0 40.61 0.9395 40.59 0.9356 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

16a,b,c 79.4 75.3 75.3 75.0 74.8 87.8 68.9 0 0 41.56 0.9612 41.53 0.9573 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

17a,b,c 80.1 75.6 75.6 75.3 75.0 88.9 68.9 0 0 42.60 0.9851 42.63 0.9823 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

18a,b,c 79.9 75.7 75.9 75.4 75.2 89.6 68.9 0 0 43.63 1.0087 43.66 1.0059 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

19a,b,c 80.0 76.0 76.0 75.7 75.4 90.8 68.9 0 0 44.71 1.0333 44.73 1.0305 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

20a,b,c 80.7 76.2 76.3 75.8 75.7 91.2 68.9 0 0 45.75 1.0559 45.57 1.0499 orange 16.410 15.850 16.080 16.120 11.210 14.110 0.930 29.89

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

Trailing-Edge Test Section With Cross-Over Jets

Lab: 165EC

Critical Venturi Throat Diameter: 0.32" 5˚ 11cross10exit

staggered

xiao huang closed

Remarks : Micro-manometer (H2O) readings should be multiplied by 2.

Date:12/28/2011 Remarks : Camera is focused on the last four cross-over holes

80 psi

DP,Turb "Hg

Pic # Tven Tin1 Tin2 Tjet Tend1 Tend2 Tamb V1 A1 V2 A2 V3 A3 Man. Liq. Pplen Psup1 Psup2 Psup3 Pend1 Pend2 DP,orifice Pamb

1a,b,c 70.7 65 65.2 65 66.8 71.9 36 0 0 32.48 0.7525 32.41 0.7485 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

2a,b,c 71.8 65.8 66 65.7 67.8 73 36 0 0 33.46 0.7761 33.55 0.7757 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

3a,b,c 71.6 66.4 66.6 66.3 68.2 73.8 36 0 0 34.72 0.8046 34.77 0.8036 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

4a,b,c 72.1 66.7 67 66.5 68.7 74.6 36 0 0 35.83 0.8303 35.88 0.829 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

5a,b,c 71.6 67.1 67.3 66.9 69 75.2 36 0 0 36.97 0.8556 36.95 0.8538 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

6a,b,c 71.4 67.3 67.5 67.1 69.3 76 36 0 0 38.14 0.8826 38.07 0.8794 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

7a,b,c 71.9 67.4 67.6 67.2 69.4 76.4 36 0 0 39.12 0.9051 39.13 0.9035 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

8a,b,c 71.5 67.4 67.6 67.2 69.5 77.2 36 0 0 40.26 0.9312 40.25 0.9291 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

9a,b,c 70.4 67.4 67.6 67.2 69.6 77.6 36 0 0 41.42 0.9579 41.39 0.9554 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

10a,b,c 70.9 67.5 67.7 67.3 69.8 78.2 36 0 0 42.44 0.9808 42.43 0.9792 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

11a,b,c 70.5 67.5 67.8 67.4 69.9 78.8 36 0 0 43.67 1.0092 43.67 1.0075 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

12a,b,c 70.6 67.5 67.7 67.4 69.9 79.4 36 0 0 44.94 1.0382 44.99 1.0377 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

13a,b,c 70.3 67.5 67.7 67.3 70 80.1 36 0 0 46.17 1.0667 46.21 1.0656 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

14a,b,c 70.5 67.5 67.8 67.4 70.1 80.8 36 0 0 47.42 1.0958 47.42 1.0932 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

15a,b,c 70.7 67.4 67.6 67.3 70 81.1 36 0 0 48.62 1.1221 48.64 1.1209 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

16a,b,c 71.1 67.5 67.7 67.4 70.1 82.5 36 0 0 49.84 1.1506 49.87 1.1484 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

17a,b,c 71.5 67.7 68 67.6 70.2 83 36 0 0 51.02 1.1773 51.07 1.176 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

18a,b,c 71 67.9 68.1 67.8 70.4 84.4 36 0 0 52.6 1.2136 52.38 1.2058 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

19a,b,c 71.6 68.1 68.4 68 70.6 85.1 36 0 0 54.12 1.2481 53.58 1.233 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

20a,b,c 71.1 68.2 68.4 68.1 70.7 86.2 36 0 0 56.09 1.2928 55.05 1.2663 orange 14.97 14.11 14.46 14.49 9.21 10.95 1.15 29.35

Cross-Over Hole Angle :

TE slot Arrangement :

Experimentalist : Bleed Valve :

Critical Venturi Inlet Pressure:

B -1

Appendix B: Source code for check.f

character*60 filename

character*80 title

character*8 PICTURES

write(6,*)'enter the name of the data file that u',

&' want to check'

read(5,10)filename

10 format(a60)

open(unit=1,file=filename,status='old')

open(unit=2,file='output.dat',status='old')

READ(1,*)NPoints,Tliquid,angle,NCO,NE,TEslots

IEND=11

do i=1,IEND

read(1,221)title

enddo

B -2

221 FORMAT(A80,//)

do i=1,NPoints

read(1,400)PICTURES

read(1,*)Pven,Tven,Tin1,Tin2,Tjet,Tend1,Tend2,Tamb,V1,A1,

&V2,A2,V3,A3,flag,Pplen,Psup1,Psup2,Psup3,Pend1,Pend2,

&Dporif,Pamb

400 FORMAT(A8)

if(Pven.lt.10.or.Pven.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Pven IN LINE #:',i,',Pven:',Pven

endif

if(DPorif.lt.0.or.DPorif1.gt.17)then

write(6,*)' '

B -3

write(6,*)'** CHECK DPorif1 in LINE #:',i,', Pven:',Pven

endif

if(Pamb.lt.28.or.Pamb.gt.31)then

write(6,*)' '

write(6,*)'** CHECK Pamb IN LINE #:',i,', Pven:',Pven

endif

if(Tamb.lt.45.or.Tamb.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Tamb IN LINE #:',i,', Pven:',Pven

endif

if(Tven.lt.45.or.Tven.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Tven IN LINE #:',i,', Pven:',Pven

endif

B -4

if(Tin1.lt.45.or.Tin1.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Tin1 IN LINE #:',i,', Pven:',Pven

endif

if(Tin1.lt.45.or.Tin2.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Tin2 IN LINE #:',i,', Pven:',Pven

endif

if(Tend1.lt.45.or.Tend1.gt.150)then

write(6,*)' '

write(6,*)'** CHECK Tend1 IN LINE #:',i,', Pven:',Pven

endif

if(Tend2.lt.45.or.Tend2.gt.150)then

B -5

write(6,*)' '

write(6,*)'** CHECK Tend2 IN LINE #:',i,', Pven:',Pven

endif

if(Tjet.lt.45.or.Tjet.gt.90)then

write(6,*)' '

write(6,*)'** CHECK Tjet IN LINE #:',i,', Pven:',Pven

endif

if(old1.eq.0)goto 31

err1=abs((v1/a1)-old1)/old1

err2=abs((v2/a2)-old2)/old2

err3=abs((v3/a3)-old3)/old3

if(err1.gt..0125)then

write(6,*)' '

B -6

write(6,*)'error in heater 1 (V or A) IN LINE #:',i

endif

if(err2.gt..0125)then

write(6,*)' '

write(6,*)'error in heater 2 (V or A) IN LINE #:',i

endif

if(err3.gt..0125)then

write(6,*)' '

write(6,*)'error in heater 3 (V or A) IN LINE #:',i

endif

31 write(6,35)PICTURES,Pven,v1/a1,v2/a2,v3/a3

write(2,35)PICTURES,Pven,v1/a1,v2/a2,v3/a3

if(flag.eq.1)goto 32

B -7

old1=v1/a1

old2=v2/a2

old3=v3/a3

flag=1.

32 continue

35 format(1x,A8,1x,f5.0,3(1x,f10.6))

enddo

write(6,*)' '

write(6,*)' '

write(6,*)' Resistances are in file : output.dat'

stop

end

C -1

Appendix C: Source code for Reduce.f

C NOTE: Tm = Tjet is used in h calculation

C FOR SULTAN AL-SHEHREY

C TRAILING-EDGE SIMULATING CHANNEL WITH CROSS-OVER SLOTS

C AND TRALING-EDGE SLOTS

C IMPINGEMENT ON A ROW OF BROKEN RADIAL RIBS

C FEBRUARY 2010

C CONTROL PANEL ARANGEMENT

C CHANNEL 1 Back Heater # 1

C CHANNEL 2 Back Heater # 2

C CHANNEL 3 Back Heater # 3

C -2

IMPLICIT REAL*8(A-H,O-Z)

CHARACTER*80 TITLE

CHARACTER*8 PICTURES

REAL*8 Mv,Nuj

COMMON TEbmax,TEbmin,TEside,TElength,Hlength,Rgas,Mv,

&Tin,Tamb,Pdown,Tliquid,TEAR

C C R I T I C A L V E N T U R I C O R R E L A T I O N

F1(A,P,T)=0.5215*A*P/SQRT(T) ! Correlation for small critial

! venturi-meters

C O R I F I C E P L A T E C O R R E L A T I O N

F2(Pf,hw,Tabs)=0.862509*K*Fa*Fh*Fm*Y1*(Dorif**2)*

&SQRT(hw*Pf*Gb/(Zf*Tabs))

C -3

Zb=0.99961

Zf=0.99958

Fa=1.00013

Fh=1.00000

Fm=1.00000

K=0.80466

Y1=0.99527

Dorif=0.6

Gb=1.

OPEN(Unit=7,FILE='output.dat',STATUS='old')

OPEN(Unit=5,FILE='uncertain.out',STATUS='old')

OPEN(Unit=9,FILE='error.out',STATUS='old')

OPEN(Unit=2,FILE='ph-in-plot.dat',STATUS='old')

OPEN(Unit=8,FILE='ph.in',STATUS='old')

OPEN(Unit=1,FILE='input.dat',STATUS='old')

C -4

Hgtopsi= 0.49083935 ! converts inches of Hg to psi

H2otopsi=Hgtopsi/13.6 ! converts inches of H2o to psi

Oiltopsi=0.826*Hgtopsi/13.6 ! converts inches of Oil to psi

FAC1=3.4121 ! converts Watts to BTU/hr

PFAC=248.8*1.4504E-04*144 ! converts inches of H2O to psf

Rgas=53.34 ! gas constant for air

FAC1=3.4121

C V E N T U R I G E O M E T R Y

C PI=3.141592..........

PI=4.*ATAN(1.E00)

C -5

Dthroat=0.32 ! 165 EGAN

Athroat=(PI/4.)*(Dthroat*Dthroat)

TElength=36.

TurbHeight=0.23

TurbWidth=0.23

TurbLength=1.32

TurbRadius=0.075

TurbGap=0.68

TurbSpacing=2.

NTurb=11

PartThick=0.9

SupHeight=4.5

SupBmin=1.1

C -6

SupBmax=1.96

SupSide=SQRT(SupHeight**2+((SupBmax-SupBmin)/2.)**2)

SupLength=49.

C H E A T E R S

Hlength=11.1 ! Spreader length

Hlength=Hlength/12. ! ft

Hwidth=2.6 ! Spreader width

Hwidth=Hwidth/12. ! ft

C T R A L I N G - E D G E C H A N N E L

TElength=36.

TEheight=2.5

C -7

TEheight=TEheight/12. ! ft

TEbmax=0.78

TEbmax=TEbmax/12. ! ft

TEbmin=0.45

TEbmin=TEbmin/12. ! ft

TEside=SQRT(TEheight**2+((TEbmax-TEbmin)/2.)**2)

TEperim=2.*TEside+TEbmax+TEbmin

TEcross=TEheight*(TEbmax+TEbmin)/2.

TEDh=4.*TEcross/TEperim

TEAR=(TEbmax+TEbmin)/(2.*TEside)

C READ IN # OF PHOTOS,LIQUID CRYSTAL REFERENCE TEMPERATURE,TILT

ANGLE,

C NUMBER OF CROSS-OVER HOLES,NUMBER OF EXIT HOLES, FLOW

ARRANGEMENT (0:INLINE, 1:STAGGERED)

READ(1,*)NP,Tliquid,angle,NCO,NE,TEslots

C -8

WRITE(8,402)NP

402 FORMAT(I5)

C C R O S S - O V E R S L O T S (I N L E T )

SLOTL=0.64

SLOTL=SLOTL/12.

SlotW=0.41

SlotW=SlotW/12.

SLotP=PI*SlotW+ 2.*(SlotL-SlotW)

SLotA=(PI/4.)*SlotW*SlotW + SlotW*(SlotL-SlotW)

SLotDH=4.*SlotA/SlotP

SlotR=0.205

SlotSpacing=2.

SoDh=SlotSpacing/(12.*SlotDh)

C -9

Zjet=1.25

ZoDh=Zjet/(12.*SlotDh)

C E X I T S L O T G E O M E T R Y

ESlotL=0.68

ESlotL=ESlotL/12.

ESlotW=0.25

ESlotW=ESlotW/12.

ESlotP=PI*ESlotW+2.*(ESlotL-ESlotW)

ESlotA=(PI/4.)*ESlotW*ESlotW+ESlotW*(ESlotL-ESlotW)

ESlotDH=4.*ESlotA/ESlotP

AreaR=(NCO*SlotA)/(NE*ESlotA)

ESlotR=0.125

C -10

ESlotSpacing=2.

write(7,999)NCO,144.*SlotA,12.*SlotP,12.*SlotDH,SlotR,SoDh,

&ZoDh,NTurb,TurbHeight,TurbWidth,TurbLength,TurbRadius,TurbGap,

&TurbSpacing,PartThick,SupHeight,SupBmin,SupBmax,SupSide,

&SupLength,12*TEheight,12*TEbmin,12*TEbmax,12*TEside,TElength,

&144.*TEcross,12.*TEDh,TEAR,NE,144.*ESlotA,12.*ESlotP,12.*ESlotDH,

&ESlotR,ESlotSpacing,AreaR,12.*Hlength,12.*Hwidth

999 format(/,

&5x,'# of Cross-Over Jets : ',i2,/,

&5x,'Inlet Slot Cross-Sectional Area',f12.6,' sq.in.',/,

&5x,'Inlet Slot Perimeter',f12.6,' inches',/,

&5x,'Inlet Slot Hydraulic Diameter',f12.6,' inches',/,

&5x,'Inlet Slot Corner Radius',f9.3,' inches',/,

&5x,'Jet Spacing, S/Dh',f6.3,/,

&5x,'Jet Spacing, Z/Dh',f6.3,/,

C -11

&5x,'# of Turbulators',I3,/,

&5x,'Turbulator Height',f6.3,' inches',/,

&5x,'Turbulator Width',f6.3,' inches',/,

&5x,'Turbulator Length',f6.3,' inches',/,

&5x,'Turbulator Corner Radius',f9.3,' inches',/,

&5x,'Turbulator Gap',f6.3,' inches',/,

&5x,'Turbulator Spacing',f6.1,' inches',/,

&5x,'Partition Wall Thickness',f6.1,' inches',/,

&5x,'Supply Channel Height',f6.1,' inches',/,

&5x,'Supply Channel Smaller Base',f6.2,' inches',/,

&5x,'Supply Channel Larger Base',f6.2,' inches',/,

&5x,'Supply Channel Side',f12.6,' inches',/,

&5x,'Supply Channel Length',f6.1,' inches',/,

&5x,'TE Channel Height',f6.1,' inches',/,

&5x,'TE Channel Smaller Base',f6.3,' inches',/,

&5x,'TE Channel Larger Base',f6.3,' inches',/,

&5x,'TE Channel Side',f12.6,' inches',/,

C -12

&5x,'TE Channel Length',f6.1,' inches',/,

&5x,'TE Channel Cross Sectional Area',f12.6,' square inches',/,

&5x,'TE Channel Hydraulic Diameter',f12.6,' inches',/,

&5x,'TE Channel Hydraulic Aspect Ratio',f12.6,' inches',/,

&5x,'# of Exit Slots : ',i2,/,

&5x,'Exit Slot Cross-Sectional Area',f12.6,' sq.in.',/,

&5x,'Exit Slot Perimeter',f12.6,' inches',/,

&5x,'Exit Slot Hydraulic Diameter',f12.6,' inches',/,

&5x,'Exit Slot Corner Radius',f6.3,' inches',/,

&5x,'Exit Slot Spacing',f6.1,' inches',/,

&5x,'Inlet-to-Exit Flow Area Ratio',f12.6,/,

&5x,'Heater Spreader Length',f6.1,' inches',/,

&5x,'Heater Spreader Width',f6.1,' inches',/)

C HEAT TRANSFER AREA

Area=Hwidth*Hlength ! sq.ft

C -13

if(TEslots.eq.0.)WRITE(7,111)Angle

if(TEslots.eq.0.)WRITE(8,111)Angle

if(TEslots.eq.1.)WRITE(7,112)Angle

if(TEslots.eq.1.)WRITE(8,112)Angle

111 FORMAT('Cross-Over Slot Angle is :', F6.1,' Degrees',///,

&'TRALING-EDGE SLOTS ARE IN-LINE',//)

112 FORMAT('Cross-Over Slot Angle is :', F6.1,' Degrees',///,

&'TRALING-EDGE SLOTS ARE STAGGERED',//)

IEND=11

DO 333 I=1,IEND

READ(1,10)TITLE

WRITE(7,10)TITLE

333 WRITE(8,10)TITLE

10 FORMAT(A80,//)

C -14

WRITE(8,450)

450 FORMAT(' PHOTO Rej Nuj hj Uncer ',//)

Reold=11200

DO 1 I=1,NP

read(1,400)PICTURES

read(1,*)Pven,Tven,Tin1,Tin2,Tjet,Tend1,Tend2,Tamb,V1,A1,

&V2,A2,V3,A3,flag,Pplen,Psup1,Psup2,Psup3,Pend1,Pend2,

&Dporif,Pamb

400 FORMAT(A8)

WRITE(7,*)' '

WRITE(7,*)' '

WRITE(7,*)' '

WRITE(7,100)PICTURES

C -15

WRITE(7,*)' '

WRITE(7,*)'Collected Data: PHOTO,Pven,Pplen,Psup1,Psup2,Psup3'

WRITE(7,*)'Pend1,Pend2,DPorif,Pamb'

WRITE(7,*)'V1,A1,V2,A2,V3,A3,Tven,Tin1,Tin2,Tjet,Tend1,Tend2,Tamb'

WRITE(7,*)' '

WRITE(7,200)PICTURES,Pven,Pplen,Psup1,Psup2,Psup3,Pend1,Pend2,DPorif,

&Pamb

WRITE(7,210)V1,A1,V2,A2,V3,A3

WRITE(7,211)Tven,Tin1,Tin2,Tend1,Tend2,Tamb

200 FORMAT(4X,A8,' ',F7.3,' ',F7.3,' ',F7.3,' ',F7.3,' ',F7.3,

&' ',F7.3,' ',F7.3,' ',F7.3,' ',F7.2)

210 FORMAT(' ',F7.2,' ',F7.4,' ',F7.2,' ',F7.4,' ',F7.2,' ',F7.4)

211 FORMAT(' ',F5.1,' ',F5.1,' ',F5.1,' ',F5.1,' ',F5.1,' ',F5.1)

Pamb =Pamb*Hgtopsi

Pdown=0.5*(Pdown1+Pdown2)

if(flag.eq.1)Pup =2*Pup*H2otopsi+Pamb ! psi

C -16

if(flag.eq.1)Pdown=2*Pdown*H2otopsi+Pamb ! psi

if(flag.eq.2)Pup =Pup*Oiltopsi+Pamb ! psi

if(flag.eq.2)Pdown=Pdown*Oiltopsi+Pamb ! psi

if(flag.eq.3)Pup =Pup*Hgtopsi+Pamb ! psi

if(flag.eq.3)Pdown=Pdown*Hgtopsi+Pamb ! psi

Tin=0.5*(Tin1+Tin2)

Tm=Tjet ! NOTE; Tm=Tjet is used for h calculation, not calculated Tm which is a few

degrees higher.

C AIR MASS FLOW RATE FROM THE CRITICAL VENTURI

Mv=F1(Athroat,Pven+Pamb,Tven+460.)

Dporif=Dporif*Oiltopsi

Pf=Dporif+Pamb

C -17

Tabs=Tend2+460.

tipmass=F2(Pf,Dporif,Tabs)

ratiof=tipmass/Mv

C TOTAL HEAT ADDED TO THE AIR BY THE HEATERS FROM THE

C INLET TO THE POINT IN QUESTION

Q=V1*A1+V2*A2+V3*A3

Q=Q*FAC1

C HEAT FLUX, BTU/(sqft.Sec)

Fluxb=V2*A2*FAC1/(Area)

CALL COEFFICIENT(Q,Fluxb,Tm,Tback,hturb,Floss,PHOTO,fluxnet)

C -18

C FILM TEMPERATURE

TF=(Tback+Tm)/2.

C DENSITY AT JET TEMPERATURE

RHO=(Pdown*144.)/(Rgas*(Tjet+460.))

C OTHER PROPERTIES AT JET TEMPERATURE

TjR=Tjet+460.

CALL AIRPROP(TjR,GAMA,CON,VIS,PR,CP)

VIS=VIS/3600.

C WRITE(6,*)' Ratio=',CON/SlotDH

C -19

C JET REYNOLDS NUMBER

Rej=4.*(Mv/NCO)/(SlotP*VIS)

C NUSSELT NUMBER

Nuj=Hturb*SlotDH/Con

C UNCERTAINTY ANALYSIS

CALL UNCERTAIN(V1,A1,V2,A2,V3,A3,

&Area,Tback,Tin,Pven+Pamb,Floss,Uncer)

WRITE(7,300)Tin,Tjet,Tm,3600*Vis,con,Mv,Rej

WRITE(7,401)Hturb,Nuj,Uncer

if((abs(Reold-Rej)/Reold).gt.0.1)WRITE(2,*)' '

WRITE(2,*)Rej,Nuj

C -20

WRITE(7,399)Pup,Pdown

WRITE(8,400)PICTURES

WRITE(8,403)Rej,Nuj,Hturb,Uncer

Reold=Rej

doverk=SlotDH/con

1 CONTINUE

403 FORMAT(1X,E11.5,1X,E11.5,1X,E11.5,1X,E9.3)

100 FORMAT(/,30X,'PHOTOS ',A8)

300 FORMAT(/,1X,'Tin=',F6.2,1X,'Tjet=',F6.2,1X,'Tm=',F6.2,1X,

&'vis=',f8.4,' lbm/hr.ft',1x,'con=',f8.4,' BTU/hr.ft.R',

&1X,'Mv=',E12.5,1x,'Rej=',F8.1)

401 FORMAT(1X,'Nuj=',F8.3,2X,' h=',F9.4,2X,

&'% Uncer (in h) =',F7.2)

399 FORMAT(1X,'Press Upstream of Slots=',F9.4,' psi',5X,

C -21

&'Test Sect Press =',F9.4,' psi',/)

STOP

END

SUBROUTINE UNCERTAIN(V1,I1,V2,I2,V3,I3,Area,Tback,Tin,

&P1,Floss,Uncer)

IMPLICIT REAL*8(A-H,O-Z)

REAL*8 I1,I2,I3

a=.220174

b=231.182609

dv1=.01

dv2=.01

dv3=.01

di1=.001

di2=.001

C -22

di3=.001

da2=1./(32.*32.)

dts=0.5

dti=0.5

dp1=0.5

Ts=Tback

Ti=Tin

FAC=491.355778

Floss=Floss/FAC

DFloss=0.1*Floss

a2=144*Area

H=(V2*I2/A2-Floss)/(Ts-Ti-(V1*I1+V2*I2+V3*I3)/(A+B*P1))

WRITE(5,*)' heat transfer coeff., h, =',H*FAC,' BUT/hr.sqft.F'

H2=H*H

C

C -23

C i2 v2

C ----- - Floss

C a2

C -----------------------------------

C i3 v3 + i2 v2 + i1 v1

C - ----------------------- + ts - ti

C b p1 + a

C

DHDI1=v1*(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/

&(b*p1+a)+ts-ti)**2)

ZI1=(DI1*DHDI1)**2

DHDV1=i1*(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/

&(b*p1+a)+ts-ti)**2)

ZV1=(DV1*DHDV1)**2

DHDI3=v3*(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/

C -24

&(b*p1+a)+ts-ti)**2)

ZI3=(DI3*DHDI3)**2

DHDV3=i3*(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/

&(b*p1+a)+ts-ti)**2)

ZV3=(DV3*DHDV3)**2

DHDI2=v2/(a2*(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti))+v2*

&(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+

&ts-ti)**2)

ZI2=(DI2*DHDI2)**2

DHDV2=i2/(a2*(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti))+i2*

&(i2*v2/a2-Floss)/((b*p1+a)*(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+

&ts-ti)**2)

ZV2=(DV2*DHDV2)**2

C -25

DHDA2=-i2*v2/(a2**2*(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti))

ZA2=(DA2*DHDA2)**2

DHDTS=-(i2*v2/a2-Floss)/(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti)**2

ZTS=(DTS*DHDTS)**2

DHDTI=(i2*v2/a2-Floss)/(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti)**2

ZTI=(DTI*DHDTI)**2

DHDP1=-b*(i2*v2/a2-Floss)*(i3*v3+i2*v2+i1*v1)/((b*p1+a)**2*

&(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti)**2)

ZP1=(DP1*DHDP1)**2

DHDFloss=-Floss/(-(i3*v3+i2*v2+i1*v1)/(b*p1+a)+ts-ti)

ZFloss=(DFloss*DFloss)**2

Uncer=100*SQRT((ZI1+ZI2+ZI3+ZV1+ZV2+ZV3+ZA2+ZTS+ZTI+

C -26

&ZP1+ZFloss)/(H2))

WRITE(5,*)' '

WRITE(5,*)' UNCERTAINTY IN HEAT TRANSFER',

&' COEFFICIENT'

WRITE(5,*)' '

WRITE(5,*)' TOTAL UNCERTAINTY % ',Uncer

WRITE(5,*)' % Uncertainty assoc. with I1',100.*sqrt(ZI1)/H

WRITE(5,*)' % Uncertainty assoc. with V1',100.*sqrt(ZV1)/H

WRITE(5,*)' % Uncertainty assoc. with I2',100.*sqrt(ZI2)/H

WRITE(5,*)' % Uncertainty assoc. with V2',100.*sqrt(ZV2)/H

WRITE(5,*)' % Uncertainty assoc. with I3',100.*sqrt(ZI3)/H

WRITE(5,*)' % Uncertainty assoc. with V3',100.*sqrt(ZV3)/H

WRITE(5,*)' % Uncertainty assoc. with A2',100.*sqrt(ZA2)/H

WRITE(5,*)' % Uncertainty assoc. with Ts',100.*sqrt(ZTS)/H

C -27

WRITE(5,*)' % Uncertainty assoc. with Tin',100.*sqrt(ZTI)/H

WRITE(5,*)' % Uncertainty assoc. with Pven',100.*sqrt(ZP1)/H

WRITE(5,*)' % Uncertainty assoc. with Floss',100.*sqrt(ZFLOSS)/H

RETURN

END

SUBROUTINE EQSOLVE(A,B,NA,NDIM,NB)

IMPLICIT REAL*8(A-H,O-Z)

DIMENSION A(NDIM,NDIM),B(NDIM,NB)

DO 291 J1=1,NA

C FIND REMAINING ROW CONTAINING LARGEST ABSOLUTE

C VALUE IN PIVOTAL COLUMN.

101 TEMP=0.

DO 121 J2=J1,NA

IF(ABS(A(J2,J1))-TEMP) 121,111,111

111 TEMP=ABS(A(J2,J1))

C -28

IBIG=J2

121 CONTINUE

IF(IBIG-J1)5001,201,131

C REARRANGING ROWS TO PLACE LARGEST ABSOLUTE

C VALUE IN PIVOT POSITION.

131 DO 141 J2=J1,NA

TEMP=A(J1,J2)

A(J1,J2)=A(IBIG,J2)

141 A(IBIG,J2)=TEMP

DO 161 J2=1,NB

TEMP=B(J1,J2)

B(J1,J2)=B(IBIG,J2)

161 B(IBIG,J2)=TEMP

C COMPUTE COEFFICIENTS IN PIVOTAL ROW.

201 TEMP=A(J1,J1)

DO 221 J2=J1,NA

221 A(J1,J2)=A(J1,J2)/TEMP

C -29

DO 231 J2=1,NB

231 B(J1,J2)=B(J1,J2)/TEMP

IF(J1-NA)236,301,5001

C COMPUTE NEW COEFFICIENTS IN REMAINING ROWS.

236 N1=J1+1

DO 281 J2=N1,NA

TEMP=A(J2,J1)

DO 241 J3=N1,NA

241 A(J2,J3)=A(J2,J3)-TEMP*A(J1,J3)

DO 251 J3=1,NB

251 B(J2,J3)=B(J2,J3)-TEMP*B(J1,J3)

281 CONTINUE

291 CONTINUE

C OBTAINING SOLUTIONS BY BACK SUBSTITUTION.

301 IF(NA-1)5001,5001,311

311 DO 391 J1=1,NB

N1=NA

C -30

321 DO 341 J2=N1,NA

341 B(N1-1,J1)=B(N1-1,J1)-B(J2,J1)*A(N1-1,J2)

N1=N1-1

IF(N1-1)5001,391,321

391 CONTINUE

5001 CONTINUE

RETURN

END

SUBROUTINE RAD(AR,Width,Length,Tback,Ttop,Tfront,Tbot,

&Frback,Frtop,Frfront,Frbot)

IMPLICIT REAL*8(A-H,O-Z)

REAL*8 Length

DIMENSION A(4,4),B(4,1),E(4),T(4),Q(4)

W=Width

H=AR*Width

H=H/Length

C -31

W=W/Length

T(1)=Tback + 460.

T(2)=Ttop + 460.

T(3)=Tfront+ 460.

T(4)=Tbot + 460.

C Emissivities

E(1)=.85 ! Liquid Crystal Foil

E(2)=.85 ! Plexiglas

E(3)=.85 ! Plexiglas

E(4)=.85 ! Plexiglas

N=4

PI=4.*ATAN(1.E00)

SIGMA=0.1712E-08

C WRITE(7,150)

C -32

150 FORMAT(//,20X,'SHAPE FACTORS',//)

C Shape Factors

F11=0.

W2=W*W

H2=H*H

Z1=1./(PI*W)

Z2=W*ATAN(1./W)

Z3=H*ATAN(1./H)

Z=SQRT(H2+W2)

Z4=-Z*ATAN(1./Z)

Z=(1.+W2)*(1.+H2)

ZZ=1.+W2+H2

ZZZ=Z/ZZ

Z=W2*ZZ/((1.+W2)*(W2+H2))

Z=Z**W2

C -33

ZZZ=ZZZ*Z

Z=H2*ZZ/((1.+H2)*(W2+H2))

Z=Z**H2

ZZZ=ZZZ*Z

Z5=.25*LOG(ZZZ)

F12=Z1*(Z2+Z3+Z4+Z5)

F14=F12

F13=1.-F11-F12-F14

F31=F13

F32=F12

F33=0.

F34=F14

DUM=W

W=H

H=DUM

C -34

W2=W*W

H2=H*H

Z1=1./(PI*W)

Z2=W*ATAN(1./W)

Z3=H*ATAN(1./H)

Z=SQRT(H2+W2)

Z4=-Z*ATAN(1./Z)

Z=(1.+W2)*(1.+H2)

ZZ=1.+W2+H2

ZZZ=Z/ZZ

Z=W2*ZZ/((1.+W2)*(W2+H2))

Z=Z**W2

ZZZ=ZZZ*Z

Z=H2*ZZ/((1.+H2)*(W2+H2))

Z=Z**H2

ZZZ=ZZZ*Z

Z5=.25*LOG(ZZZ)

C -35

F21=Z1*(Z2+Z3+Z4+Z5)

F22=0.

F23=F21

F24=1.-F21-F22-F23

F41=F21

F42=F24

F43=F23

F44=0.

C

C WRITE(7,110)F11,F12,F13,F14

C WRITE(7,120)F21,F22,F23,F24

C WRITE(7,130)F31,F32,F33,F34

C WRITE(7,140)F41,F42,F43,F44

C

110 FORMAT(5X,'F11=',F6.4,5X,'F12=',F6.4,5X,'F13=',F6.4,

&5X,'F14=',F6.4,/)

C -36

120 FORMAT(5X,'F21=',F6.4,5X,'F22=',F6.4,5X,'F23=',F6.4,

&5X,'F24=',F6.4,/)

130 FORMAT(5X,'F31=',F6.4,5X,'F32=',F6.4,5X,'F33=',F6.4,

&5X,'F34=',F6.4,/)

140 FORMAT(5X,'F41=',F6.4,5X,'F42=',F6.4,5X,'F43=',F6.4,

&5X,'F44=',F6.4,//)

C WRITE(7,160)

160 FORMAT(/,20X,'EMISSIVITIES',//)

C WRITE(7,100)(I,E(I),I=1,N)

C WRITE(7,170)

170 FORMAT(/,20X,'TEMPERATURES IN R',//)

C WRITE(7,100)(I,T(I),I=1,N)

A(1,1)=F11-1./(1.-E(1))

A(1,2)=F12

A(1,3)=F13

A(1,4)=F14

C -37

A(2,1)=F21

A(2,2)=F22-1./(1.-E(2))

A(2,3)=F23

A(2,4)=F24

A(3,1)=F31

A(3,2)=F32

A(3,3)=F33-1./(1.-E(3))

A(3,4)=F34

A(4,1)=F41

A(4,2)=F42

A(4,3)=F43

A(4,4)=F44-1./(1.-E(4))

C WRITE(7,180)

180 FORMAT(//,20X,'COEFFICIENT MATRIX',/)

C -38

C WRITE(7,200)((A(I,J),J=1,N),I=1,N)

DO I=1,N

B(I,1)=-E(I)*SIGMA*(T(I)**2.)*(T(I)**2.)/(1.-E(I))

ENDDO

C WRITE(7,250)

C WRITE(7,100)(I,B(I,1),I=1,N)

200 FORMAT(1X,4E15.6)

250 FORMAT(/,20X,'RIGHT HAND SIDE ',/)

C WRITE(7,55)

55 FORMAT(//,20X,'GAUSSIAN ELIMINATION METHOD',/)

CALL EQSOLVE(A,B,N,N,1)

C WRITE(7,50)

C WRITE(7,100)(I,B(I,1),I=1,N)

DO I=1,N

Q(I)=E(I)*(SIGMA*(T(I)**2.)*(T(I)**2.)-B(I,1))/(1.-E(I))

ENDDO

C -39

Frback= q(1)

Frtop= q(2)

Frfront=q(3)

Frbot= q(4)

C WRITE(7,350)

C WRITE(7,100)(I,Q(I),I=1,N)

100 FORMAT(4(I3,E15.6))

50 FORMAT(/,20X,'RADIOCITIES',/)

350 FORMAT(/,20X,'HEAT FLUXES IN BTU/hr.sqft',/)

RETURN

END

SUBROUTINE COEFFICIENT(Q,Fluxb,Tm,Tback,hback,Floss,PHOTO,fluxnet)

IMPLICIT REAL*8(A-H,O-Z)

REAL*8 kinc,kadh,kkap,kmyl,kpoly,ksty,kblack,kliq,kplex,

&Length,Mv

C -40

COMMON Bmax,Bmin,Width,Length,Hlength,Rgas,Mv,

&Tin,Tamb,Pdown,Tliquid,AR

C B A C K W A L L (LIQUID CRYSTAL WALL)

C FROM THE CENTER OF HEATING ELEMENT TO THE AMBIENT AIR

C 0.25 mil INCONEL HEATING ELEMENT ----- 0.5 mil ADHESIVE ----- 0.5 mil

C KAPTON ---- 2 mil ADHESIVE ----- 1.625 inches POLYURETHANE ----

C 2.0 inches STYROFOAM ---- AMBIENT

C tinc1/kinc -- tadh1/kadh -- tkap1/kkap -- tadh4/kadh -- tpoly/kpoly

C -- tsty/ksty -- 1/ho

C FROM THE CENTER OF HEATING ELEMENT TO THE AIR INSIDE THE TEST

SECTION

C -41

C 0.25 mil INCONEL HEATING ELEMENT ----- 1.0 mil ADHESIVE ----- 2.0 mil

C KAPTON ---- 1.0 mil ADHESIVE ----- 0.5 mil INCONEL SPREADER ---- 1.0 mil

C ADHESIVE ---- 2.0 mil KAPTON ---- 1.5 mil ADHESIVE ---- 3.0 mil

C ABSORPTIVE BLACK BACKGROUND ---- 2.0 mil LIQUID CRYSTAL ---- 5.0 mil

C MYLAR ---- AIR INSIDE THE TEST SECTION

C tinc1/kinc -- tadh2/kadh -- tkap2/kkap -- tadh2/kadh -- tinc2/kinc --

C tadh2/kadh -- tkap2/kkap -- tadh3/kadh -- tblack/kblack -- tliq/kliq --

C tmyl/kmyl -- 1/hi

C F R O N T W A L L (CAMERA SIDE)

C TOTAL RESISTANCE

C -42

C AIR INSIDE THE TEST SECTION ---- 0.45 inches PLEXIGLAS ---- AMBIENT

C 1/hi -- tplex/kplex -- 1/ho

C Heat transfer coefficient on the outer surface

De=7./12. ! ft, test section side with insulation

TambR=Tamb+460.

CALL AIRPROP(TambR,Gama,CON,VIS,PR,CP)

ho=0.36*con/De ! Ozisik, Page 443

tinc1 = 0.25e-03/12. ! MINCO's fact sheet

tinc2 = 0.50e-03/12.

C -43

tadh1 = 0.5e-03/12. ! MINCO's fact sheet

tadh2 = 1.0e-03/12.

tadh3 = 1.5e-03/12.

tadh4 = 2.0e-03/12.

tkap1 = 0.5e-03/12. ! MINCO's fact sheet

tkap2 = 2.0e-03/12.

tpoly = 3./12.

tplex = 0.5/12.

tsty = 2./12.

tblack = 3.0e-03/12. ! absorptive black background (from DAVIS)

tliq = 2.0e-03/12. ! liquid crystal thickness (from DAVIS)

C -44

tmyl = 5.0e-03/12. ! MYLAR thickness (from DAVIS)

kkap = 0.0942 ! BTU/hr.ft.F MINCO (0.163 W/m.K) agrees with

! Sam Spring's 0.095 BTU/hr.ft.F

ksty = 0.02 ! BTU/hr.ft.F Sam Spring

kpoly = 0.0333 ! BTU/hr.ft.F from GOLDENWEST INC. R=2.5-2.75

! hr.(sqft)/BTU.in

kplex = 0.11 ! BTU/hr.ft.F AIN Plastics k=1.3 BTU/hr.F.sqft/in,

! same given by 1-800-523-7500

kmyl = 0.085 ! BTU/hr.ft.F Abauf's serpentine report, page 19

kadh = 0.1272 ! BTU/hr.ft.F MINCO (0.220 W/m.K)

kinc = 9.0152 ! BTU/hr.ft.F MINCO (inconel 600 K=15.6 W/m.K)

kblack = 0.165 ! BTU/hr.ft.F Glycerin

kliq = 0.165 ! BTU/hr.ft.F Glycerin

Rinc1 = tinc1/kinc

C -45

Rinc2 = tinc2/kinc

Radh1 = tadh1/kadh

Radh2 = tadh2/kadh

Radh3 = tadh3/kadh

Radh4 = tadh4/kadh

Rkap1 = tkap1/kkap

Rkap2 = tkap2/kkap

Rpoly = tpoly/kpoly

Rsty = tsty/ksty

Rplex= tplex/kplex

Rblack = tblack/kblack

C -46

Rliq = tliq/kliq

Rmyl = tmyl/kmyl

C write(6,*)Rmyl

Rconv = 1./ho

Rback = 0.5*Rinc1 + Radh1 + Rkap1 + Radh4 + Rpoly + Rconv

Rfront =0.5*Rinc1 + Radh2 + Rkap2 + Radh2 + Rinc2 + Radh2 +

&Rkap2 + Radh3 + Rblack + Rliq

Fluxtop=0.

Fluxf=0.

Fluxbot=0.

C -47

Theater = (fluxb+Tamb/Rback+Tliquid/Rfront)/

&(1./Rback+1./Rfront)

C loss from the back side

flback = (Theater-Tamb)/Rback

ffront = (Theater-Tliquid)/Rfront

C Surface temperature, Ts

C write(6,*)'tmyl, kmyl,Rmyl,ffront, DT',12*tmyl,kmyl,Rmyl,ffront,ffront*Rmyl

C write(6,*)'DT',ffront*Rmyl

Tback= Tliquid -ffront*Rmyl

Tf=0.5*(Tm+Tback)

perloss=100.*(flback/fluxb)

WRITE(7,*)' '

C -48

WRITE(7,*)' LIQUID CRYTAL SIDE'

WRITE(7,*)' '

WRITE(7,101)Theater,fluxb,flback,ffront,

& perloss,Tliquid,Tback,Tamb,ho

100 FORMAT(/,5X,'HEATER TEMPERATURE = ',F8.3,' F',/,

&5X,'TOTAL HEAT FLUX = ',F8.3,' BTU/hr.sqft',/,

&5X,'HEAT FLUX TO THE BACK = ',F8.3,' BTU/hr.sqft',/,

&5X,'HEAT FLUX TO THE FRONT = ',F8.3,' BTU/hr.sqft',/,

&5X,'% OF HEAT LOST FROM THE BACK SIDE = ',F8.3,/,

&5X,'LIQUID CRYSTAL TEMPERATURE = ',F8.3,' F',/,

&5X,'SURFACE TEMPERATURE = ',F8.3,' F',/,

&5X,'AMBIENT TEMPERATURE = ',F8.3,' F',/,

&5X,'Uinf where camera is located= ',F8.3,' ft/s',/,

&5X,'Re based on the test section outer dimension= ',E13.6,/,

&5X,'Outer heat transfer coefficient= ',F8.3,

&' BTU/hr.sqft.F')

101 FORMAT(/,5X,'HEATER TEMPERATURE = ',F8.3,' F',/,

C -49

&5X,'TOTAL HEAT FLUX = ',F8.3,' BTU/hr.sqft',/,

&5X,'HEAT FLUX TO THE BACK = ',F8.3,' BTU/hr.sqft',/,

&5X,'HEAT FLUX TO THE FRONT = ',F8.3,' BTU/hr.sqft',/,

&5X,'% OF HEAT LOST FROM THE BACK SIDE = ',F8.3,/,

&5X,'LIQUID CRYSTAL TEMPERATURE = ',F8.3,' F',/,

&5X,'SURFACE TEMPERATURE = ',F8.3,' F',/,

&5X,'AMBIENT TEMPERATURE = ',F8.3,' F',/,

&5X,'Outer heat transfer coefficient= ',F8.3,

&' BTU/hr.sqft.F')

Abot= 3.*Bmax*Hlength

Atop= 3.*Bmin*Hlength

Aback =3.*Width*Hlength

Afront=Aback

! AIR INLET PROPERTIES

C -50

TinR=Tin+460.

CALL AIRPROP(TinR,gamin,CONin,VISin,PRin,CPin)

! FLUX LOSSES FROM TOP, BOTTOM AND FRONT WALLS

! T O P W A L L

C Rtop=Rplex+Rconv

Ttop=Tm

C Fltop=(Ttop-Tamb)/Rtop ! Losses from top

! B O T T O M W A L L

C Rbot=Rplex+Rsty+Rconv

C -51

Tbot=Tin

C Flbot=(Tbot-Tamb)/Rbot

! F R O N T W A L L

R1=Rplex+Rconv !from surface to ambient

! INITIAL GUESSES

hback=(Fluxb-Flback)/(Tback-Tm)

hfront=hback

Tfront=Tm

DO I = 1,20

C -52

R3=1./hfront !convective resistance

! RADIATIONAL LOSSES

call rad(AR,Width,Length,Tback,Ttop,Tfront,Tbot,

&Frback,Frtop,Frfront,Frbot)

TfrontN=((1./R3)*Tm+(1./R1)*Tamb-Frfront)/((1./R1)+(1./R3))

IF(ABS(TfrontN-Tfront).LE.0.001) GO TO 999

Tfront=TfrontN

Flfront=(Tfront-Tamb)/R1

Flbot=0. ! For this geometry

Fltop=0. ! For this geometry

C -53

! TOTAL HEAT LOSS TO THE AMBIENT

Qwaste=Fltop*Atop+Flbot*Abot+Flfront*Afront+Flback*Aback

! NET HEAT ADDED TO THE AIR FROM THE INLET TO THE POINT IN

QUESTION

Qadd = Q-Qwaste

! AIR MIXED MEAN ENTHALPY AT THE POINT WHERE THE HEAT TRANSFER

! COEFFICIENT IS BEING MEASURED

TmCAL=Tin+(Qadd)/(3600.*Mv*CPin) ! Energy balance

! HEAT TRANSFER COEFFICIENT FROM THE NEWTON LAW OF COOLING

C -54

Floss=Flback+Frback

hback=(Fluxb-Flback-Frback)/(Tback-Tm)

hfront=hback

ENDDO

WRITE(7,*)' did not convergance after 20 iterations'

GO TO 998

999 WRITE(7,*)' convergance after',I,' iterations'

998 write(7,110)Tback,Ttop,Tfront,Tbot

110 FORMAT(5x,'Back, Top, Front and Botom Wall Temperatures: ',

&/,10x,4F10.2,' F')

C For CFD use

fluxnet=(Fluxb-Flback-Frback)

C

write(7,115)TmCAL,Tf

115 FORMAT(5X,'Cal. Air Mixed Mean and Film Temperatures',2F9.3,' F')

C -55

write(7,170)Q

170 format(5x,'Total Elect. Power=',F8.3,' BTU/hr')

write(7,116)Qwaste

116 FORMAT(5X,'Total Heat Loss to Ambient=',F8.3,' BTU/hr')

write(7,190)Fluxb,Fluxtop,Fluxf,Fluxbot

190 FORMAT(5X,'Heat Fluxes Generated by Back, Top, Front and'

&,' Bottom Heaters:',/,5x,4F11.3,' BTU/sqft.hr')

write(7,180)Flback,Fltop,Flfront,Flbot

180 FORMAT(5X,'Flux Losses from Back, Top, Front and'

&,' Bottom Surfaces:',/,10x,4F13.3,' BTU/sqft.hr')

write(7,150)Frback,Frtop,Frfront,Frbot

150 FORMAT(5X,'Radiative Fluxes from Back, Top, Front and'

&,' Bottom Surfaces:',/,10x,4F10.3,' BTU/sqft.hr')

RETURN

END

subroutine AIRPROP(t,gamx,kx,mux,prx,cpx)

C -56

IMPLICIT REAL*8(A-H,O-Z)

c physical properties of dry air at one atmosphere

c ref: ge heat transfer handbook

c

c temperature range: 160 to 3960 deg. rankine

c -300 to 3500 deg. fahreinheit

c

c t - temperature, R

c gamx - ratios of specific heats

c kx - thermal conductivity, BTU/hr.ft.R

c mux - viscosity, lbm/hr.ft

c prx - prandtl no.

c cpx - specific heat, BTU/lbm.R

c

c

dimension tab(34),gam(34),pr(34),cp(34)

C -57

real*8 k(34),mu(34),kx,mux

data nent/34/

data tab/ 160., 260.,

& 360., 460., 560., 660., 760., 860., 960., 1060.,

& 1160., 1260., 1360., 1460., 1560., 1660., 1760., 1860.,

& 1960., 2060., 2160., 2260., 2360., 2460., 2560., 2660.,

& 2760., 2860., 2960., 3160., 3360., 3560., 3760., 3960./

data gam/ 1.417, 1.411,

& 1.406, 1.403, 1.401, 1.398, 1.395, 1.390, 1.385, 1.378,

& 1.372, 1.366, 1.360, 1.355, 1.350, 1.345, 1.340, 1.336,

& 1.332, 1.328, 1.325, 1.321, 1.318, 1.315, 1.312, 1.309,

& 1.306, 1.303, 1.299, 1.293, 1.287, 1.281, 1.275, 1.269/

data k/ 0.0063,0.0086,

& 0.0108,0.0130,0.0154,0.0176,0.0198,0.0220,0.0243,0.0265,

& 0.0282,0.0301,0.0320,0.0338,0.0355,0.0370,0.0386,0.0405,

& 0.0422,0.0439,0.0455,0.0473,0.0490,0.0507,0.0525,0.0542,

& 0.0560,0.0578,0.0595,0.0632,0.0666,0.0702,0.0740,0.0780/

C -58

data mu/ 0.0130,0.0240,

& 0.0326,0.0394,0.0461,0.0519,0.0576,0.0627,0.0679,0.0721,

& 0.0766,0.0807,0.0847,0.0882,0.0920,0.0950,0.0980,0.1015,

& 0.1045,0.1075,0.1101,0.1110,0.1170,0.1200,0.1230,0.1265,

& 0.1300,0.1330,0.1360,0.1420,0.1480,0.1535,0.1595,0.1655/

data pr/ 0.7710,0.7590,

& 0.7390,0.7180,0.7030,0.6940,0.6860,0.6820,0.6790,0.6788,

& 0.6793,0.6811,0.6865,0.6880,0.6882,0.6885,0.6887,0.6890,

& 0.6891,0.6893,0.6895,0.6897,0.6899,0.6900,0.6902,0.6905,

& 0.6907,0.6909,0.6910,0.6913,0.6917,0.6921,0.6925,0.6929/

data cp/ 0.247, 0.242,

& 0.241, 0.240, 0.241, 0.242, 0.244, 0.246, 0.248, 0.251,

& 0.254, 0.257, 0.260, 0.264, 0.267, 0.270, 0.272, 0.275,

& 0.277, 0.279, 0.282, 0.284, 0.286, 0.288, 0.291, 0.293,

& 0.296, 0.298, 0.300, 0.305, 0.311, 0.318, 0.326, 0.338/

c

c

C -59

if(t.lt.tab(1)) print 510,t,tab(1)

510 format(" in airprop --- temp=",f8.1," is less than min temp",

&" of ",f8.1)

if(t.gt.tab(nent)) print 520, t,tab(nent)

520 format(" in airprop --- temp=",f8.1," is greater than max",

&" temp of ",f8.1)

if(t-tab(1))120,120,100

100 if(tab(nent)-t)130,130,110

110 m=2

go to 140

120 j=1

go to 180

130 j=nent

go to 180

140 if(t-tab(m))160,170,150

150 m=m+1

go to 140

C -60

c

c -- Linear Interpolation ---

c

160 slp=(t-tab(m-1))/(tab(m)-tab(m-1))

mux= mu(m-1)+(mu(m)-mu(m-1))*slp

prx= pr(m-1)+(pr(m)-pr(m-1))*slp

cpx=cp(m-1)+(cp(m)-cp(m-1))*slp

kx=k(m-1)+(k(m)-k(m-1))*slp

gamx=gam(m-1)+(gam(m)-gam(m-1))*slp

go to 190

170 j=m

go to 180

180 mux=mu(j)

prx=pr(j)

cpx=cp(j)

kx=k(j)

gamx=gam(j)

C -61

190 return

end

c

D -1

Appendix D: Source code for Integarea.f

REAL Nu,Nuave

CHARACTER*80 TITLE

CHARACTER*8 PICTURES

open(unit=1,file='ph.in',status='old')

open(unit=2,file='area.dat',status='old')

open(unit=7,file='pl.dat',status='old')

open(unit=8,file='Nuave-plot.dat',status='old')

open(unit=9,file='have-plot.dat',status='old')

write(6,*)' WHICH AREA DO YOU WANT TO INTEGRATE?'

write(6,*)' '

read *, area

READ(1,*)NP

DO I=1,14

READ(1,100)TITLE

ENDDO

100 FORMAT(A80,//)

D -2

N=0

2 N=N+1

Reo=Re

IF(N.GT.NP) GO TO 3

read(2,400)PICTURES

400 FORMAT(A8)

if(area.eq.1)READ(2,*)A

if(area.eq.2)READ(2,*)dum,A

if(area.eq.3)READ(2,*)dum,dum,A

if(area.eq.4)READ(2,*)dum,dum,dum,A

if(area.eq.5)READ(2,*)dum,dum,dum,dum,A

if(area.eq.6)READ(2,*)dum,dum,dum,dum,dum,A

if(area.eq.7)READ(2,*)dum,dum,dum,dum,dum,dum,A

if(area.eq.8)READ(2,*)dum,dum,dum,dum,dum,dum,dum,A

if(area.eq.9)READ(2,*)dum,dum,dum,dum,dum,dum,dum,dum,A

D -3

read(1,400)PICTURES

READ(1,*)Re,Nu,h,Uncer

IF(N.EQ.1) THEN

J=1

SUMRe=0.

SUMNu=0.

SUMh=0.

SUMunc=0.

SUMA=0.

GO TO 4

ENDIF

DIFF=ABS((Re-Reo)/Re)

IF(DIFF.GE..09)THEN

3 JTOT=J

J=1

Reave=SUMRe/JTOT

Nuave=SUMNu/SUMA

D -4

have=SUMh/SUMA

Uncave=SUMunc/JTOT

WRITE(6,300)Reave,Nuave,have,Uncave,SUMA,JTOT

WRITE(7,300)Reave,Nuave,have,Uncave,SUMA,JTOT

WRITE(8,301)Reave,Nuave,have/Nuave

WRITE(9,301)Reave,have,have/Nuave

300 FORMAT(1X,5E12.5,I4)

301 FORMAT(1X,3E12.5)

IF(N.GT.NP) GO TO 99

SUMRe=0.

SUMNu=0.

SUMh=0.

SUMunc=0.

SUMA=0.

ELSE

J=J+1

D -5

ENDIF

4 SUMRe=SUMRe+Re

SUMNu=SUMNu+Nu*A

SUMh =SUMh +h*A

SUMunc=SUMunc+Uncer

SUMA=SUMA+A

GO TO 2

99 WRITE(6,200)

WRITE(7,200)

200 FORMAT(5X,'Re',10X,'Nu',13X,'h',7X,'Uncer',

&9X,'Atot',5x,'# OF POINTS',/)

REWIND 1

READ(1,*)NP

DO I=1,14

READ(1,100)TITLE

WRITE(7,100)TITLE

ENDDO

D -6

STOP

END

D -7