mark claywell donald horkheimer garrett stockburger university of minnesota

24
Investigation of Intake Concepts for a Formula SAE Four-Cylinder Engine Using 1D/3D (Ricardo WAVE-VECTIS) Coupled Modeling Techniques Mark Claywell Donald Horkheimer Garrett Stockburger University of Minnesota

Upload: tamar

Post on 05-Feb-2016

60 views

Category:

Documents


0 download

DESCRIPTION

Investigation of Intake Concepts for a Formula SAE Four-Cylinder Engine Using 1D/3D (Ricardo WAVE-VECTIS) Coupled Modeling Techniques. Mark Claywell Donald Horkheimer Garrett Stockburger University of Minnesota. Agenda. Background Motivation Design Method - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

Investigation of Intake Concepts for a Formula SAE Four-Cylinder

Engine Using 1D/3D (Ricardo WAVE-VECTIS) Coupled Modeling

Techniques

Mark Claywell Donald Horkheimer Garrett Stockburger

University of Minnesota

Page 2: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

2

Agenda • Background• Motivation • Design Method• Simulation Methods and Assumptions• Grid Convergence Study• Results• Flow Visualization• Improved Understanding Through Issues

Raised By Simulation • Conclusion

2006-01-3652

Page 3: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

3

Background

• Student Design Competition

•Events in America, Australia, Brazil, Germany, Italy, Japan, United Kingdom

•200+ Universities involved

•Team score based on sales presentation, cost report, design quality, acceleration time, fuel economy, skid-pad, auto-cross and endurance race

University of Minnesota SAE Engine

• Yamaha YZF-R6, Four Cylinder, Four stroke

• 600cc Displacement• 15,500 rpm redline• Bore = 65.5mm, Stroke =

44.5mm• 4-2-1 Exhaust Header• Sequential Port Fuel Injection

(student calibrated)• DOHC, 4 valves per cylinder• Compression Ratio = 12.4:1• Fuel – Gasoline, 100 Octane

2006-01-3652

Page 4: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

4

Motivation – Where to begin?

2006-01-3652

Page 5: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

5

Design Process

2006-01-3652

State Needs

DefineSpecifications

GenerateConcepts

Evaluate & Select

DetailedDesign

Manufacture& Test

State Needs

DefineSpecifications

GenerateConcepts

Evaluate & Select

DetailedDesign

Manufacture& Test

Main Focus of Paper

Page 6: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

6

Concepts vs Designs

2006-01-3652

Concepts

Designs

Page 7: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

7

Making Concepts ComparableGeometric Similarities•Inlet box to diffuser exit is identical•Restrictor geometry identical•Plenum volume kept constant•Runner length, diameter, and taper kept constant•Packaging bend angle held at 55°

Page 8: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

8

Ricardo WAVE and VECTIS Simulation Software

2006-01-3652

WAVE (1D) VECTIS (3D)

•Intake to Tail-Pipe Engine Code

•Easily provides realistic boundary conditions to CFD solver

•Uses simple models to analyze complex problems

•Provides actionable engine performance information

•Quick simulation time

•Off the shelf

•Computational Fluid Dynamics (CFD) Code – More Accurate Flow Results

•Integrated pre/post-processing and solver

•Automatic mesh generator works with CAD derived geometry

•Automotive specific solver modules

•Easy to implement parallel solver

•Off the shelf

Guessing at CFD boundary conditions is no good!

WAVE makes the use of VECTIS for intake design worthwhile

No code coupling = Questionable fidelity

Page 9: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

9

Why Not a Steady State CFD Approach? Agreement between flow solutions is poor•Steady state cylinder balance didn’t match•Steady state didn’t result in shocks, unsteady did•Finding non-tuning design improvements with steady state CFD may still be possible

2006-01-3652

Page 10: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

10

Simplifying Assumptions Assumptions•WAVE-VECTIS junctions placed in 1D flow areas•No throttle body•No fuel spray particles in CFD domain•k-ε turbulence model

2006-01-3652

Inlet Box

Page 11: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

11

Grid Convergence Study Grid convergence studies• ASME, AIAA, and others require it. Good practice.

2006-01-3652

rff

ff

pln

12

23ln

1][

pr

EsFdForFineGriGCI

%1001

12

f

ffE

Page 12: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

12

Results – Total Volumetric Efficiency Predictions

•Differences in total VE from concept to concept is small•VE curves can be made similar by varying intake dimensions

2006-01-3652

Page 13: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

13

Results – Volumetric Efficiency

2006-01-3652

Page 14: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

14

Results – Absolute Average Deviation of Volumetric Efficiency (I)•Total volumetric efficiency hides the superiority of the best intake concept•Individual cylinder to cylinder imbalance needs to be measured to identify best concept

N

ii xx

NAAD

1

1

2006-01-3652

Page 15: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

15

Results – Absolute Average Deviation of Volumetric Efficiency (II)

2006-01-3652

Conical-Spline Intake Concept (With Straight Runners)

A
Graphs look really skinny and quirky. Maybe just copy and past into separate graphs and put into presentation. Then you can size them as you like. The left side looks especially weird.
Page 16: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

16

Results – Improvements in Calibration Process and Radiated Sound

2006-01-3652

Page 17: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

17

Results – Choked Flow Insights and Post Diffuser Total Pressure Recovery

Diffuser Exit

•Lower AAD results in more regular pressure pulses at throat and lower time of choked flow

•Beyond a certain diffuser length/area ratio total pressure recovery is limited

2006-01-3652

Side Entry Intake Conical Intake

A
Make Mach graphs appear to be same sizeNeed easy to see labels on the two Mach plots, so we don't forget during the presentation. And it makes it easier for people to see. Maybe have a label "Side Entry" and "Conical-Spline". No one will be able to read the text above the plots. Would also like to see the same pressure loss graph (to the right) for the Top Feed intake, too.
Page 18: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

18

Flow Visualization – Enhanced Understanding

2006-01-3652

•Look at air and fuel cylinder to cylinder stealing

•Identify regions of pressure loss and flow separation

A
I think the graph on the upper right hand is pretty uninteresting and obvious, and generally not noteworthy.You mention region of separation. Could you show one in the restrictor and perhaps another one elsewhere. In the intake manifold proper, the ISE intake would be the best candidate.
Page 19: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

19

Flow Visualization – Enhanced Understanding II

14,000 RPM

11,500 RPM

14,000 RPM

11,500 RPM

Page 20: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

20

Time Averaged Velocity – 14,000 RPM

Page 21: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

21

Velocity Normal to Plane – Time Averaged14,000 RPM

Page 22: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

22

Flow Visualization – Flow Dynamics Through Animation

2006-01-3652

14,000 RPM 14,000 RPM

Page 23: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

23

ConclusionLooked at how plenum geometry determines

performance using WAVE-VECTIS• Found grid convergence studies essential for

good CFD• Conical intake stood out as best

• Smallest cylinder to cylinder imbalance• Better AFR control and acoustic characteristics

• Regular pressure pulses at throat reduce choked flow• Adding bent runners for realistic packaging hurt

performance, but only slightly• Improved understanding of fluid flow and

dynamics

2006-01-3652

Page 24: Mark Claywell  Donald Horkheimer  Garrett Stockburger University of Minnesota

24

Questions?

Acknowledgements• Ricardo Sponsorship and Support - Patrick Niven &

Karl John• University of Minnesota Supercomputer Institute - Dr.

H. Birali Runesha and Support Staff• University of Minnesota SAE Chapter - Dr. Patrick Starr

and Dr. David Kittleson• Minnesota State University, Mankato - Dr. Bruce Jones

2006-01-3652