choked flow of gases

4
P.O. BOX Q • TRUMBULL, CT 06611 • CT PHONE (203) 261-6711 • TOLL FREE PHONE (800) 533-3285 • FAX (203) 261-8331 © O'KEEFE CONTROLS CO. • 2000 ALL RIGHTS RESERVED e-mail [email protected] website www.okcc.com Choked Flow of Gases When the air velocity reaches sonic velocity (P 2 /P 1 .528) further increases in P 1 (upstream pressure) do not cause any further increase in the air velocity through the orifice. Conse- quently it is wrongly concluded that the mass flow rate also does not increase. As the air pressure (P 1 ) increases, the density of the air also increases; and since the mass flow rate is also a function of density, the mass flow rate increases linearly with pressure (P 1 ). Even though the air velocity through the orifice is limited to the speed of sound, the mass flow rate continues to increase as the absolute pressure (P 1 ) increases. What is Choked? The parameter that becomes “choked” or “limited” is the velocity of the air. It is more accurate to use the term “choked velocity” rather than “choked flow” when the absolute pressure ratio of air through an orifice is .528. Vacuum Conditions Air at atmospheric pressure enters the orifice and flows to a downstream vacuum pump. In the case of vacuum conditions on the outlet of an orifice and where the inlet is at ambient atmospheric pressure, both the air velocity and the mass flow rate become choked (limited) when sonic velocity is achieved through the orifice. For atmospheric inlet pressure and downstream vacuum, both the air velocity and mass flow rate are limited. The Basic Concept A greatly misunderstood and misapplied notion is that of “choked flow”, also referred to as “critical flow”. In gas flow through an orifice there is an occa- sion where the gas velocity reaches sonic conditions. This occurs for air flow when the absolute pressure ratio is .528, i.e. when the downstream absolute pressure (P 2 ) is 52.8% of the upstream absolute pressure (P 1 ). Sonic velocity occurs for air flow when P 2 /P 1 .528. The air flow velocity is limited once the absolute pressure ratio is .528. For air flow through an orifice with an inlet air temperature of 68 o F the choked (sonic) velocity is 1129 ft/sec. The Misconception! Once sonic velocity is achieved in orifice air flow (P 2 /P 1 = .528), it is easy to "assume" that the mass flow rate is constant for all pressure ratios less than .528; i.e. P 2 /P 1 .528. For example, when P 2 is 14.7 psia and P 1 is 27.84 psia, sonic velocity occurs through the orifice. As P 1 further increases there is no further increase in the velocity of the air flowing through the orifice. Conditions for the onset of sonic velocity in orifice air flow. Consider all the Factors! The mass flow rate through an orifice is a func- tion of three basic parameters. Q (flow) is a function of • Velocity • Density • Orifice Area The reason for the mass flow rate limitation is the fixed inlet density combined with the fixed velocity. The flow charts on pages 16-18 show the choked mass flow effect for vacuum con- ditions. At vacuum levels between 15-30” Hg the mass flow rate is fixed. Choked Flow for Positive Pressure Conditions As in the case of the above vacuum conditions there are certain situations in which choked flow does occur for positive (above atmo- spheric) pressure. By maintaining a fixed in- let pressure to the orifice and allowing the outlet pressure (back pressure) to vary, there is a range of outlet pressures over which the mass flow rate is fixed. For example (see chart below). With an inlet pressure of 80 psig, the mass flow rate is choked (limited) for all outlet pressures less than 35.30 psig (including vacuum conditions). The actual flow rate is constant for the outlet pressure range of 35.30 psig to as low as a complete vacuum. The flow rate can be obtained from the charts on pages 16-18; e.g. for an orifice of .010" diam- eter and with 80 psig inlet pressure, the choked flow rate is 8.4 scfh (page 16). This flow rate will be constant for all outlet pressure conditions between 35.30 psig and full vacuum. 0 1 .528 Sonic Velocity Mass Flow Rate Air Velocity 0 0 Mass Flow Rate Air Velocity Sonic Velocity Conditions – Air Flow Outlet Pressure Inlet Pressure For Sonic Velocity Gage Absolute Absolute Gage Pressure Pressure Pressure Pressure psig psia psia psig 100 114.7 60.56 45.86 90 104.7 55.28 40.58 80 94.7 50.00 35.30 70 84.7 44.72 30.02 60 74.7 39.44 24.74 50 64.7 34.16 19.46 40 54.7 28.88 14.18 30 44.7 23.60 8.90 20 34.7 18.32 3.62 15 29.7 15.68 .98 14.7 29.4 15.52 .82 10 24.7 13.08 -1.62 5 19.7 10.40 -4.30 1 15.7 8.29 -6.47 0 14.7 7.76 -6.94 Temperature 68°F P2 = 14.7 psia = 0 psig P2 /P1 – Absolute Pressure Ratio 0 1 .528 Sonic Velocity 1129 ft/sec @ 68° F Choked Flow Choked Velocity Mass Flow Rate 0 P 2 /P 1 – Absolute Pressure Ratio Air Velocity P 1 = 14.7 psia P 2 < P 1 Vacuum P 1 = 14.7 psia = 0 psig Standard Atmospheric Conditions P 1 = 27.84 psia = 13.14 psig P 2 = 14.7 psia = 0 psig Sonic Velocity Through Orifice TUTORIAL 0 1 .528 Sonic Velocity 1129 ft/sec @ 68° F Air velocity is constant in this region Air Velocity 0 P 2 /P 1 – Absolute Pressure Ratio P 1 P 2 38

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Page 1: Choked Flow of Gases

P.O. BOX Q • TRUMBULL, CT 06611 • CT PHONE (203) 261-6711 • TOLL FREE PHONE (800) 533-3285 • FAX (203) 261-8331

© O'KEEFE CONTROLS CO. • 2000 ALL RIGHTS RESERVED e-mail [email protected] • website www.okcc.com

Choked Flow of Gases

When the air velocity reaches sonic velocity(P2/P1 ≤ .528) further increases in P1 (upstreampressure) do not cause any further increase inthe air velocity through the orifice. Conse-quently it is wrongly concluded that the massflow rate also does not increase.

As the air pressure (P1) increases, the densityof the air also increases; and since the massflow rate is also a function of density, the massflow rate increases linearly with pressure (P1).

Even though the air velocity through the orifice is limitedto the speed of sound, the mass flow rate continues toincrease as the absolute pressure (P1) increases.

What is Choked?The parameter that becomes “choked” or“limited” is the velocity of the air. It is moreaccurate to use the term “choked velocity”rather than “choked flow” when the absolutepressure ratio of air through an orifice is≤ .528.

Vacuum Conditions

Air at atmospheric pressure enters the orifice and flowsto a downstream vacuum pump.

In the case of vacuum conditions on the outletof an orifice and where the inlet is at ambientatmospheric pressure, both the air velocityand the mass flow rate become choked(limited) when sonic velocity is achievedthrough the orifice.

For atmospheric inlet pressure and downstream vacuum,both the air velocity and mass flow rate are limited.

The Basic ConceptA greatly misunderstood and misappliednotion is that of “choked flow”, also referredto as “critical flow”.

In gas flow through an orifice there is an occa-sion where the gas velocity reaches sonicconditions. This occurs for air flow when theabsolute pressure ratio is .528, i.e. when thedownstream absolute pressure (P2) is 52.8%of the upstream absolute pressure (P1).

Sonic velocity occurs for air flow whenP2

/P1 ≤ .528.

The air flow velocity is limited once the absolutepressure ratio is ≤ .528.

For air flow through an orifice with aninlet air temperature of 68oF the choked(sonic) velocity is 1129 ft/sec.

The Misconception!Once sonic velocity is achieved in orifice airflow (P2/P1 = .528), it is easy to "assume" thatthe mass flow rate is constant for all pressureratios less than .528; i.e. P2/P1 ≤ .528. Forexample, when P2 is 14.7 psia and P1

is 27.84psia, sonic velocity occurs through the orifice.As P

1 further increases there is no further

increase in the velocity of the air flowingthrough the orifice.

Conditions for the onset of sonic velocity in orifice air flow.

Consider all the Factors!The mass flow rate through an orifice is a func-tion of three basic parameters.

Q (flow) is a function of• Velocity• Density• Orifice Area

The reason for the mass flow rate limitation isthe fixed inlet density combined with the fixedvelocity. The flow charts on pages 16-18 showthe choked mass flow effect for vacuum con-ditions. At vacuum levels between 15-30” Hgthe mass flow rate is fixed.

Choked Flow for PositivePressure ConditionsAs in the case of the above vacuum conditionsthere are certain situations in which chokedflow does occur for positive (above atmo-spheric) pressure. By maintaining a fixed in-let pressure to the orifice and allowing theoutlet pressure (back pressure) to vary, thereis a range of outlet pressures over which themass flow rate is fixed.

For example (see chart below).

• With an inlet pressure of 80 psig, the massflow rate is choked (limited) for all outletpressures less than 35.30 psig (includingvacuum conditions).

• The actual flow rate is constant for theoutlet pressure range of 35.30 psig to aslow as a complete vacuum. The flow ratecan be obtained from the charts on pages16-18; e.g. for an orifice of .010" diam-eter and with 80 psig inlet pressure, thechoked flow rate is 8.4 scfh (page 16). Thisflow rate will be constant for all outletpressure conditions between 35.30 psigand full vacuum.

0 1 .528

Sonic Velocity

Mass FlowRate

Air Velocity 0➔➔➔➔➔ 0

MassFlow Rate

➔➔➔➔ ➔ AirVelocity

➔➔➔➔ ➔

Sonic Velocity Conditions – Air Flow Outlet PressureInlet Pressure

For Sonic VelocityGage Absolute Absolute Gage

Pressure Pressure Pressure Pressurepsig psia psia psig100 114.7 ≤ 60.56 ≤ 45.8690 104.7 ≤ 55.28 ≤ 40.5880 94.7 ≤ 50.00 ≤ 35.3070 84.7 ≤ 44.72 ≤ 30.0260 74.7 ≤ 39.44 ≤ 24.7450 64.7 ≤ 34.16 ≤ 19.4640 54.7 ≤ 28.88 ≤ 14.1830 44.7 ≤ 23.60 ≤ 8.9020 34.7 ≤ 18.32 ≤ 3.6215 29.7 ≤ 15.68 ≤ .98

14.7 29.4 ≤ 15.52 ≤ .8210 24.7 ≤ 13.08 ≤ -1.625 19.7 ≤ 10.40 ≤ -4.301 15.7 ≤ 8.29 ≤ -6.470 14.7 ≤ 7.76 ≤ -6.94

Temperature 68°F

P2 = 14.7 psia = 0 psig

P2 /P1 – Absolute Pressure Ratio

0 1 .528

Sonic Velocity1129 ft/sec @

68°F

Choked FlowChoked Velocity

MassFlow Rate

➔➔➔➔ ➔

➔➔➔➔➔ 0

P2 /P1 – Absolute Pressure Ratio

AirVelocity

➔➔➔➔ ➔

P1 = 14.7 psia

P2 < P1Vacuum

P1 = 14.7 psia = 0 psig

StandardAtmosphericConditions

P1 = 27.84 psia = 13.14 psig

P2 = 14.7 psia = 0 psig

Sonic VelocityThrough Orifice

TUTORIAL

0 1 .528

Sonic Velocity1129 ft/sec @

68°F

Air velocity isconstant inthis region

AirVelocity

➔➔➔➔ ➔

➔➔➔➔➔ 0

P2 /P1 – Absolute Pressure Ratio

P1 P2

38

Page 2: Choked Flow of Gases

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914

818

720

7 2

44 2

6730

734

336

239

442

845

8 5

09 5

38 6

04 6

3869

3 7

63 8

39 8

9210

2111

2580

9310

311

011

912

713

113

714

516

721

023

1 2

7329

834

338

440

544

348

151

357

0 6

04 6

7871

677

885

694

310

0011

4612

6390

106

115

122

132

141

146

151

161

185

231

256

303

331

379

424

447

489

532

568

631

670

750

792

860

947

1042

1106

1267

1398

100

114

126

135

146

156

164

167

177

203

254

282

331

362

415

468

496

540

587

627

697

739

831

875

951

1047

1153

1225

1403

1545

510

.411

.412

.313

.314

.314

.515

.416

.319

.2 2

3.9

26.4

31.

4 3

6.2

42.4

47.7

50.6

55.

160

.064

.070

.376

.184

.988

.6 9

6.1

104

114

123

138

150

1013

.114

.415

.416

.617

.618

.019

.2 2

0.3

23.6

29.4

32.7

38.6

44.

9 5

1.7

57.6

63.

468

.974

.879

.987

.994

.910

611

012

013

014

215

317

318

715

13.8

15.2

16.2

17.4

18.3

18.8

20.0

21.1

24.

530

.533

.739

.446

.854

.060

.266

.171

.878

.083

.591

.799

.011

011

512

513

514

816

018

019

520

13.8

15.2

16.2

17.4

18.3

18.8

20.0

21.1

24.5

30.5

33.7

39.4

46.8

54.

060

.266

.171

.878

.0 8

3.5

91.7

99.0

110

115

125

135

148

160

180

195

3013

.815

.216

.217

.418

.318

.8 2

0.0

21.1

24.5

30.5

33.7

39.4

46.8

54.0

60.

266

.171

.878

.0 8

3.5

91.

799

.011

011

512

513

514

816

018

019

5

Vacuum LevelIn. Hg.

Sta

nd

ard

Co

nd

itio

ns

70

°F,

14

.7 p

sia

SC

FH

– S

tan

da

rd C

u.

Ft.

Pe

r H

ou

rA

bo

ve d

ata

ob

tain

ed

with

Typ

e B

re

stri

cto

r. F

low

ra

tes

for

oth

er

me

tal r

est

rict

ors

are

SL

PM

– S

tan

da

rd L

iters

Pe

r M

inu

tee

sse

ntia

lly t

he

sa

me

as

for

Typ

e B

. A

bo

ve d

ata

su

pe

rce

de

s p

revi

ou

s p

ub

lica

tion

s.

Page 3: Choked Flow of Gases

17

Met

al O

rific

e A

ir F

low

– S

LPM

Orif

ice

Dia

met

er0.

004

0.00

50.

006

0.00

70.

008

0.00

90.

010

0.01

10.

012

0.01

30.

014

0.01

50.

016

0.01

70.

018

0.01

90.

020

0.02

10.

022

0.02

30.

024

0.02

50.

026

0.02

70.

028

0.02

90.

031

0.03

20.

033

Inch

es

Siz

eN

umbe

r4

56

78

910

1112

1314

1516

1718

1920

2122

2324

2526

2728

2931

3233

Cv

0.00

035

0.00

061

0.00

086

0.00

120.

0015

0.00

190.

0025

0.00

280.

0034

0.00

380.

0043

0.00

500.

0055

0.00

670.

0073

0.00

800.

0088

0.00

960.

011

0.01

20.

013

0.01

40.

016

0.01

70.

018

0.01

90.

022

0.02

40.

025

10.

035

0.06

40.

086

0.12

70.

170

0.22

60.

280

0.30

80.

398

0.45

0.52

0.61

0.66

0.77

0.86

0.96

1.05

1.13

1.29

1.41

1.54

1.67

1.91

1.95

2.21

2.39

2.65

2.88

3.03

50.

090.

160.

210.

300.

400.

520.

650.

710.

921.

061.

211.

411.

541.

761.

982.

222.

472.

652.

973.

243.

53 3

.83

4.34

4.44

4.94

5.31

5.86

6.42

6.80

100.

120.

220.

310.

430.

570.

740.

931.

011.

291.

481.

681.

952.

012.

262.

542.

833.

163.

534.

334.

755.

185.

556.

156.

437.

187.

838.

639.

409.

9815

0.16

0.28

0.39

0.54

0.72

0.93

1.17

1.26

1.62

1.85

2.10

2.44

2.50

2.85

3.23

3.57

4.01

4.41

5.35

5.93

6.43

6.95

7.58

7.95

8.78

9.58

10.6

11.6

12.3

200.

190.

330.

460.

650.

851.

101.

381.

491.

922.

192.

492.

872.

973.

403.

864.

264.

845.

226.

356.

957.

588.

158.

909.

2810

.311

.212

.413

.514

.325

0.22

0.39

0.53

0.75

0.98

1.27

1.59

1.71

2.20

2.50

2.86

3.28

3.42

3.92

4.45

4.91

5.59

6.01

7.30

7.95

8.65

9.38

10.2

10.7

11.7

12.8

14.2

15.4

16.3

300.

250.

440.

600.

851.

121.

431.

801.

932.

472.

823.

213.

693.

874.

435.

035.

566.

336.

818.

238.

989.

7510

.611

.512

.013

.214

.415

.917

.318

.440

0.30

0.54

0.74

1.05

1.38

1.77

2.21

2.37

3.04

3.45

3.93

4.51

4.78

5.47

6.21

6.85

7.81

8.42

10.1

11.0

12.0

13.0

14.1

14.7

16.1

17.5

19.4

21.1

22.5

500.

360.

650.

881.

261.

652.

102.

622.

803.

584.

074.

645.

315.

706.

517.

408.

159.

2610

.011

.913

.014

.215

.416

.617

.319

.020

.722

.925

.026

.660

0.42

0.75

1.02

1.46

1.91

2.42

3.02

3.23

4.13

4.70

5.34

6.13

6.61

7.56

8.58

9.46

10.7

11.6

13.8

15.0

16.4

17.7

19.2

20.0

21.9

23.8

26.4

28.8

30.7

700.

480.

861.

161.

672.

172.

753.

433.

664.

685.

326.

056.

967.

538.

619.

7710

.812

.213

.215

.617

.018

.520

.121

.722

.724

.827

.030

.032

.734

.980

0.54

0.96

1.30

1.87

2.43

3.08

3.83

4.09

5.23

5.95

6.77

7.79

8.46

9.67

11.0

12.1

13.7

14.9

17.5

19.0

20.7

22.5

24.2

25.3

27.7

30.2

33.6

36.7

39.0

900.

601.

071.

44 2

.08

2.69

3.40

4.23

4.51

5.7

86.

587.

49 8

.62

9.38

10.7

12.2

13.4

15.2

16.5

19.3

21.0

22.

924

.9 2

6.8

28.0

30.7

33.5

37.

240

.643

.210

00.

66 1

.17

1.58

2.2

82.

953.

724.

634.

94 6

.33

7.22

8.21

9.46

10.3

11.8

13.4

14.7

16.6

18.0

21.1

23.0

25.1

27.

429

.430

.833

.736

.840

.944

.647

.55

0.05

30.

096

0.12

90.

191

0.25

30.

332

0.40

60.

450

0.58

20.

661

0.7

730.

899

0.97

71.

141.

281.

411.

551.

701.

902.

10 2

.30

2.48

2.74

2.83

3.16

3.41

3.78

4.12

4.32

10

0.06

90.

124

0.16

80.

246

0.32

40.

421

0.51

90.

564

0.73

00.

834

0.97

21.

12 1

.24

1.41

1.5

81.

791.

962.

182.

442.

682.

893.

133.

443.

584.

004.

304.

775.

165.

4315

0.07

50.

134

0.1

850.

268

0.35

10.

455

0.56

60.

614

0.79

2 0

.902

1.07

1.22

1.35

1.5

51.

751.

942.

19 2

.32

2.6

12.

853.

12 3

.34

3.65

3.78

4.20

4.51

5.05

5.4

55.

7220

0.07

50.

134

0.1

850.

268

0.35

10.

455

0.56

60.

614

0.79

20.

902

1.07

1.22

1.35

1.55

1.75

1.94

2.19

2.32

2.6

12.

853.

123.

343.

653.

784.

204.

515.

055.

455.

7230

0.07

50.

134

0.18

50.

268

0.35

10.

455

0.56

60.

614

0.79

20.

902

1.07

1.22

1.35

1.55

1.75

1.94

2.19

2.32

2.61

2.8

53.

123.

343.

653.

784.

20 4

.51

5.05

5.45

5.72

Supply Pressure – psig

Choked Flow

Vacuum LevelIn. Hg. Supply Pressure – psig

Choked Flow

Orif

ice

Dia

met

er0.

035

0.03

70.

038

0.03

90.

040

0.04

10.

042

0.04

30.

047

0.05

20.

055

0.06

00.

063

0.06

70.

070

0.07

30.

076

0.07

90.

081

0.08

60.

089

0.09

40.

096

0.10

00.

104

0.10

90.

113

0.12

00.

125

Inch

es

Siz

eN

umbe

r35

3738

3940

4142

4347

52

55 6

063

6770

7376

7981

8689

9496

100

104

109

113

120

125

Cv

0.02

80.

031

0.0

320.

033

0.03

60.

038

0.03

90.

041

0.04

80.

059

0.06

80.

081

0.08

80.

100.

110.

120.

13 0

.14

0.15

0.17

0.18

0.20

0.21

0.2

3 0

.25

0.27

0.31

0.34

0.37

13.

483.

834.

13 4

.46

4.60

4.67

4.99

5.36

6.4

38.

049.

4011

.212

.214

.215

.916

.918

.520

.321

.723

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.428

.430

.132

.935

.539

.643

.147

.850

.15

7.67

8.48

9.0

99.

7010

.210

.611

.312

.114

.217

.620

.3 2

3.9

26.1

30.3

33.

836

.139

.443

.146

.0 5

1.1

54.9

61.9

65.0

70.8

76.6

84.8

92.

110

210

810

10.6

11.8

12.5

13.6

14.4

14.8

15.6

16.8

19.4

24.

527

.132

.235

.240

.745

.648

.552

.957

.361

.667

.9 7

2.3

81.0

85.5

92.3

102

112

118

135

148

1513

.114

.515

.416

.717

.718

.219

.120

.4 2

3.6

29.7

32.9

39.0

42.6

49.3

55.

358

.864

.069

.474

.582

.187

.397

.810

311

112

313

514

316

317

820

15.3

17.0

18.1

19.6

20.9

21.

422

.524

.027

.735

.0 3

8.7

45.9

50.1

58.0

65.0

69.0

75.3

81.4

87.3

95.6

102

114

121

130

144

158

167

190

210

2517

.719

.620

.822

.624

.024

.725

.927

.631

.940

.344

.652

.857

.766

.774

.779

.386

.493

.510

011

011

713

113

814

916

418

019

121

924

130

20.0

22.

223

.625

.627

.228

.029

.431

.336

.045

.650

.459

.765

.275

.484

.389

.597

.410

511

312

513

214

815

616

818

520

421

624

827

340

24.8

27.4

31.7

31.6

33.6

34.6

36.3

38.7

44.5

56.3

62.2

73.6

80.3

92.

710

411

012

012

913

915

316

218

119

120

722

825

126

730

633

750

29.5

32.

634

.837

.640

.141

.343

.346

.052

.966

.974

.087

.495

.411

012

313

114

215

316

418

119

2 2

1522

724

727

2 2

9931

736

440

160

34.3

38.0

40.6

43.8

46.7

48.1

50.3

53.5

61.5

77.7

85.8

101

110

127

142

151

164

177

189

210

223

250

264

286

315

347

368

422

465

7039

.243

.346

.350

.053

.3 5

5.0

57.4

61.

070

.088

.497

.611

512

614

516

217

118

620

221

624

025

428

530

132

736

039

642

148

253

180

44.0

48.

752

.156

.260

.061

.9 6

4.5

68.5

78.6

99.1

109

129

141

162

181

191

209

227

242

269

285

320

338

367

404

445

472

541

596

9050

.054

.2 5

7.8

62.4

66.7

68.9

71.5

76.0

87.2

109

121

143

156

179

200

211

231

251

268

298

316

354

374

406

447

492

522

598

660

100

53.9

59.6

63.7

68.7

73.5

77.3

78.6

83.5

95.8

120

133

156

171

196

221

234

255

277

296

329

349

392

413

449

494

544

578

662

729

54.

925.

405.

816.

296.

766.

827.

297.

679.

0811

.312

.414

.817

.120

.0 2

2.5

23.9

26.0

28.

330

.233

.235

.940

.141

.845

.349

.053

.957

.965

.370

.910

6.18

6.78

7.29

7.8

58.

318.

509.

089.

5811

.113

.915

.418

.221

.224

.427

.229

.9 3

2.5

35.3

37.7

41.5

44.8

50.0

52.1

56.6

61.2

67.2

72.2

81.4

88.4

156.

507.

177.

638.

228.

668.

879.

4610

.011

.614

.415

.918

.622

.125

.528

.431

.233

.936

.839

.443

.346

.752

.154

.459

.063

.870

.175

.384

.992

.220

6.50

7.1

77.

638.

228.

66 8

.87

9.46

10.0

11.6

14.4

15.9

18.6

22.1

25.5

28.4

31.2

33.9

36.8

39.4

43.3

46.7

52.1

54.4

59.0

63.8

70.1

75.3

84.9

92.2

306.

50 7

.17

7.63

8.22

8.66

8.87

9.46

10.0

11.6

14.4

15.9

18.6

22.1

25.5

28.4

31.2

33.9

36.8

39.4

43.3

46.7

52.1

54.4

59.0

63.8

70.1

75.3

84.9

92.2

Vacuum LevelIn. Hg.

Sta

nd

ard

Co

nd

itio

ns

70

°F,

14

.7 p

sia

SC

FH

– S

tan

da

rd C

u.

Ft.

Pe

r H

ou

rA

bo

ve d

ata

ob

tain

ed

with

Typ

e B

re

stri

cto

r. F

low

ra

tes

for

oth

er

me

tal r

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rict

ors

are

SL

PM

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da

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iters

Pe

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inu

tee

sse

ntia

lly t

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sa

me

as

for

Typ

e B

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ve d

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su

pe

rce

de

s p

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ou

s p

ub

lica

tion

s.

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Page 4: Choked Flow of Gases

18

P

.O.

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.okc

c.co

m

Sap

phire

Orif

ice

Air

Flo

w –

SLP

MO

rific

eD

iam

eter

0.00

120.

0016

0.00

200.

0024

0.00

280.

0031

0.00

350.

0039

0.00

430.

0047

0.00

510.

0055

0.00

590.

0063

0.00

670.

0071

0.00

790.

0087

0.00

940.

0102

0.01

100.

0118

0.01

260.

0134

0.01

420.

0157

0.01

730.

0189

0.02

050.

0213

0.02

280.

0252

Inch

es

Size

Num

ber

34

56

78

910

1112

1314

1516

1718

2022

2426

2830

3234

3640

4448

5254

5864

Cv

0.00

0030

0.00

0053

0.00

0090

0.00

012

0.00

017

0.00

022

0.00

028

0.00

035

0.00

042

0.00

050

0.00

061

0.00

071

0.00

084

0.00

094

0.00

110.

0012

0.00

150.

0018

0.00

210.

0024

0.00

280.

0032

0.00

360.

0040

0.00

460.

0057

0.00

670.

0080

0.00

910.

010

0.01

10.

013

10.

003

0.00

50.

010

0.01

40.

020

0.02

50.

034

0.04

00.

050

0.05

80.

068

0.08

00.

095

0.10

60.

120

0.13

90.

161

0.19

40.

259

0.27

50.

300

0.34

00.

393

0.44

60.

499

0.67

70.

822

0.96

51.

101.

121.

381.

69

50.

009

0.01

30.

027

0.03

60.

047

0.05

90.

076

0.09

30.

108

0.13

60.

159

0.19

20.

223

0.25

60.

273

0.31

30.

350

0.43

00.

584

0.62

30.

695

0.80

00.

933

1.06

1.20

1.51

1.81

2.16

2.50

2.57

3.26

4.06

100.

010

0.01

60.

036

0.04

90.

065

0.08

20.

107

0.13

20.

164

0.19

30.

228

0.26

40.

308

0.35

70.

382

0.43

00.

480

0.59

00.

830

0.86

80.

968

1.09

1.27

1.45

1.63

2.01

2.43

2.90

3.32

3.45

4.43

5.58

150.

014

0.02

10.

046

0.06

20.

082

0.10

40.

134

0.16

60.

205

0.24

00.

285

0.32

90.

386

0.44

30.

482

0.53

50.

613

0.75

51.

051.

111.

241.

421.

631.

852.

092.

563.

083.

694.

264.

435.

557.

0820

0.01

60.

025

0.05

50.

074

0.09

90.

125

0.15

90.

197

0.24

30.

284

0.33

70.

390

0.45

70.

525

0.56

90.

635

0.73

00.

910

1.25

1.32

1.48

1.70

1.95

2.20

2.48

3.04

3.64

4.36

5.06

5.31

6.55

8.33

250.

019

0.03

00.

063

0.08

70.

115

0.14

40.

184

0.22

90.

280

0.32

70.

389

0.45

00.

526

0.60

50.

654

0.73

30.

843

1.05

1.44

1.52

1.70

1.95

2.24

2.52

2.84

3.50

4.19

5.03

5.81

6.11

7.53

9.55

300.

022

0.03

40.

072

0.09

80.

132

0.16

40.

208

0.26

00.

317

0.37

00.

440

0.51

10.

595

0.68

50.

710

0.83

80.

958

1.19

1.63

1.69

1.91

2.19

2.52

2.84

3.19

3.96

4.75

5.69

6.57

6.90

8.48

10.7

400.

027

0.04

30.

089

0.12

20.

163

0.20

30.

257

0.32

10.

390

0.45

60.

543

0.63

20.

734

0.84

50.

880

1.04

1.18

1.47

2.02

2.11

2.35

2.67

3.07

3.46

3.90

4.89

5.86

7.02

8.10

8.50

10.4

13.1

500.

032

0.05

20.

106

0.14

70.

195

0.24

10.

306

0.38

30.

463

0.54

20.

652

0.75

30.

872

1.00

1.05

1.24

1.41

1.75

2.39

2.50

2.78

3.16

3.63

4.08

4.59

5.83

6.96

8.35

9.63

10.1

12.3

15.5

600.

037

0.06

10.

123

0.17

10.

227

0.28

00.

356

0.44

50.

536

0.63

00.

751

0.87

51.

011.

161.

231.

451.

642.

032.

772.

893.

203.

634.

174.

695.

296.

778.

109.

6911

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.9

700.

042

0.07

00.

141

0.19

50.

259

0.31

80.

403

0.50

70.

609

0.71

70.

855

0.99

61.

151.

321.

401.

661.

872.

313.

143.

283.

624.

124.

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719.

2311

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800.

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0.08

00.

158

0.20

00.

292

0.35

70.

453

0.56

90.

683

0.80

40.

959

1.12

1.28

1.48

1.57

1.86

2.09

2.59

3.51

3.66

4.04

4.68

5.28

5.93

6.69

8.65

10.4

12.3

14.3

14.8

17.9

22.6

900.

053

0.08

90.

175

0.24

40.

324

0.39

60.

502

0.63

20.

757

0.89

11.

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241.

421.

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322.

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894.

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475.

075.

836.

567.

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100

0.05

80.

098

0.19

30.

269

0.35

60.

435

0.55

10.

692

0.83

00.

978

1.17

1.36

1.56

1.80

1.92

2.27

2.55

3.15

4.26

4.44

4.89

5.57

6.38

7.18

8.12

10.6

12.6

15.0

17.2

18.0

21.6

27.3

50.

003

0.00

60.

014

0.02

00.

028

0.03

60.

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0.05

70.

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0.08

50.

100

0.11

60.

137

0.15

60.

169

0.19

90.

229

0.27

70.

377

0.40

10.

451

0.51

00.

591

0.67

30.

764

0.98

21.

161.

381.

611.

642.

132.

61

10

0.00

40.

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0.01

80.

027

0.03

60.

046

0.06

10.

073

0.09

30.

109

0.12

80.

149

0.17

50.

200

0.21

70.

253

0.29

20.

352

0.48

20.

503

0.55

60.

638

0.73

40.

833

0.95

51.

261.

511.

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112.

553.

19

150.

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0.01

0 0

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00.

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0.07

90.

100

0.1

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138

0.15

90.

188

0.21

40.

235

0.26

90.

320

0.39

00.

525

0.55

40.

626

0.71

10.

818

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312.

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48

200.

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100

0.11

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90.

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40.

235

0.26

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320

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00.

525

0.55

40.

626

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10.

818

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312.

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48

300.

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00.

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0.03

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0.07

90.

100

0.11

70.

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0.15

90.

188

0.21

40.

235

0.26

90.

320

0.39

00.

525

0.55

40.

626

0.71

10.

818

0.92

11.

071.

391.

651.

992.

312.

392.

773.

48

Supply Pressure – psig

Choked Flow

Supply Pressure – psig

Choked Flow

Orif

ice

Dia

met

er0.

0012

0.00

160.

0020

0.00

240.

0028

0.00

310.

0035

0.00

390.

0043

0.00

470.

0051

0.00

550.

0059

0.00

630.

0067

0.00

710.

0079

0.00

870.

0094

0.01

020.

0110

0.01

180.

0126

0.01

340.

0142

0.01

570.

0173

0.01

890.

0205

0.02

130.

0228

0.02

52

Inch

es

Siz

eN

umbe

r3

45

67

89

1011

1213

1415

1617

1820

2224

2628

3032

3436

4044

4852

5458

64

Cv

0.00

0030

0.00

0053

0.00

0090

0.00

012

0.00

017

0.00

022

0.00

028

0.00

035

0.00

042

0.00

050

0.00

061

0.00

071

0.00

084

0.00

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0.00

110.

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150.

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210.

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0.00

280.

0032

0.00

360.

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0.00

460.

0057

0.00

670.

0080

0.00

910.

010

0.01

10.

013

10.

007

0.01

10.

021

0.03

00.

042

0.05

30.

072

0.08

50.

106

0.12

30.

144

0.16

90.

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0.22

50.

254

0.29

40.

341

0.41

10.

549

0.58

30.

636

0.72

00.

833

0.94

51.

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431.

742.

042.

332.

372.

923.

58

50.

019

0.02

70.

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0.07

50.

100

0.12

40.

161

0.19

70.

228

0.28

80.

337

0.40

70.

471

0.54

20.

577

0.66

30.

740

0.91

11.

241.

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982.

252.

533.

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834.

585.

305.

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908.

60

100.

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0.03

40.

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0.10

40.

138

0.17

40.

227

0.28

00.

347

0.40

90.

483

0.55

90.

653

0.75

60.

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0.91

11.

021.

251.

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312.

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454.

265.

156.

147.

037.

319.

3911

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150.

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0.04

40.

097

0.13

10.

174

0.22

00.

284

0.35

20.

434

0.50

80.

604

0.69

70.

818

0.93

91.

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131.

301.

602.

222.

352.

633.

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453.

924.

435.

426.

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829.

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3911

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0.03

40.

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0.11

70.

157

0.21

00.

265

0.33

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417

0.51

50.

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0.71

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826

0.96

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111.

211.

351.

551.

932.

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143.

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256.

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719.

2410

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250.

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0.06

40.

133

0.18

40.

244

0.30

50.

390

0.48

50.

593

0.69

30.

824

0.95

31.

111.

281.

391.

551.

792.

223.

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223.

604.

134.

755.

346.

027.

428.

8810

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.916

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.2

300.

046

0.07

20.

152

0.20

80.

280

0.34

70.

441

0.55

10.

672

0.78

40.

932

1.08

1.26

1.45

1.50

1.78

2.03

2.52

3.45

3.58

4.05

4.64

5.34

6.02

6.76

8.39

10.1

12.1

13.9

14.6

18.0

22.7

400.

057

0.09

10.

189

0.25

80.

345

0.43

00.

544

0.68

00.

826

0.96

61.

151.

341.

561.

791.

862.

202.

503.

114.

284.

474.

985.

666.

507.

338.

2610

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.917

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.8

500.

068

0.11

00.

225

0.31

10.

413

0.51

10.

648

0.81

10.

981

1.15

1.38

1.60

1.85

2.13

2.22

2.63

2.99

3.71

5.06

5.30

5.89

6.69

7.69

8.64

9.72

12.4

14.7

17.7

20.4

21.4

26.1

32.8

600.

079

0.12

90.

261

0.36

20.

481

0.59

30.

754

0.94

31.

141.

331.

591.

852.

142.

462.

613.

073.

474.

305.

876.

126.

787.

698.

839.

9411

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.317

.220

.523

.524

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.137

.9

700.

089

0.14

90.

299

0.41

30.

549

0.67

40.

854

1.07

1.29

1.52

1.81

2.11

2.43

2.80

2.97

3.52

3.96

4.89

6.65

6.95

7.67

8.73

10.0

11.3

12.7

16.3

19.6

23.3

26.9

28.2

33.9

42.8

800.

100

0.16

80.

335

0.42

40.

619

0.75

60.

960

1.21

1.45

1.70

2.03

2.37

2.72

3.13

3.33

3.94

4.43

5.49

7.44

7.75

8.56

9.75

11.2

12.6

14.2

18.3

22.0

26.1

30.3

31.4

37.9

47.9

900.

111

0.18

80.

371

0.51

70.

686

0.83

91.

061.

341.

601.

892.

252.

623.

013.

473.

714.

364.

926.

088.

248.

589.

4710

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.8

100

0.12

20.

208

0.40

90.

570

0.75

40.

922

1.17

1.47

1.76

2.07

2.47

2.88

3.30

3.81

4.07

4.81

5.40

6.67

9.03

9.41

10.4

11.

813

.515

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.222

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.836

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.8

50.

007

0.01

30.

029

0.04

30.

059

0.07

60.

100

0.12

10.

154

0.18

00.

212

0.24

60.

290

0.33

10.

358

0.42

20.

485

0.58

70.

799

0.85

00.

956

1.08

1.25

1.43

1.62

2.08

2.46

2.92

3.41

3.47

4.51

5.53

100.

009

0.01

80.

039

0.05

70.

076

0.09

80.

128

0.15

50.

197

0.23

10.

271

0.31

60.

371

0.42

40.

460

0.53

60.

619

0.74

61.

021.

071.

181.

351.

561.

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364.

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76

150.

012

0.02

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0.06

30.

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0.10

70.

138

0.16

80.

212

0.24

80.

292

0.33

70.

398

0.45

30.

498

0.57

00.

678

0.82

61.

111.

171.

331.

511.

731.

952.

262.

953.

504.

224.

895.

065.

877.

37

200.

012

0.02

00.

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0.06

30.

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0.10

70.

138

0.16

80.

212

0.24

80.

292

0.33

70.

398

0.45

30.

498

0.57

00.

678

0.82

61.

111.

171.

331.

511.

731.

952.

262.

953.

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224.

895.

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877.

37

300.

012

0.02

00.

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0.06

30.

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0.10

70.

138

0.16

80.

212

0.24

80.

292

0.33

70.

398

0.45

30.

498

0.57

00.

678

0.82

61.

111.

171.

331.

511.

731.

952.

262.

953.

504.

224.

895.

065.

877.

37

Vacuum LevelIn. Hg.

Sta

nd

ard

Co

nd

itio

ns

70

°F,

14

.7 p

sia

SC

FH

– S

tan

da

rd C

u.

Ft.

Pe

r H

ou

rA

bo

ve d

ata

ob

tain

ed

with

Typ

e S

re

stri

cto

r. F

low

ra

tes

for

Typ

e A

, B

TF

, B

WF

, F

, J,

SL

PM

– S

tan

da

rd L

iters

Pe

r M

inu

teL

, P

, a

nd

SF

re

stri

cto

rs a

re e

sse

ntia

lly t

he

sa

me

as

for

Typ

e S

.A

bo

ve d

ata

su

pe

rce

de

s p

revi

ou

s p

ub

lica

tion

s.

Sap

phire

Orif

ice

Air

Flo

w –

SC

FH

Vacuum LevelIn. Hg.