Unsteady flow simulation of a high lift trapezoidal wing using a lattice boltzmann method

38th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2008, Pages

  Satti, Rajani ^a   Li, Yanbing ^a   Shock, Richard ^a   Noelting, Swen ^a  

^a EXA CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC FORCES; ANGLES OF ATTACK; CFD CODES; CFD SIMULATIONS; EXPERIMENTAL DATABASE; EXPERIMENTAL MEASUREMENTS; IN-DEPTH ANALYSIS; LATTICE BOLTZMANN METHOD; LOCAL FLOW STRUCTURE; MEAN FLOW FIELDS; REALISTIC GEOMETRY; SIGNIFICANT IMPACTS; SPANWISE DISTRIBUTION; SURFACE PRESSURES; THREE DIMENSIONAL SIMULATIONS; TIME-DEPENDENT; WING MODELS;

ANGLE OF ATTACK; DROP FORMATION; FLOW FIELDS; FLOW SIMULATION; FLUID DYNAMICS; FORECASTING; NASA; OPTICAL TRANSFER FUNCTION; THREE DIMENSIONAL; THREE DIMENSIONAL COMPUTER GRAPHICS; UNSTEADY FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78049523834     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (36)

1. Van Dam C.P., "The Aerodynamic Design of Multi-Element High-Lift Systems for Transport Airplanes" Progress in Aerospace Sciences, Vol.38, pp.101-144, 2002.
2. Rudolph PKC, "High-lift systems on commercial subsonic airliners," NASA CR 4746, September 1996.
3. Meredith P. "Viscous phenomena affecting high-lift systems and suggestions for future CFD development" High-Lift System Aerodynamics, AGARD CP 515, September 1993. p.19-1-19-8.
4. Rudnik, R and Geyr, H., "The European High Lift Project EUROLIFT II-Objectives, Approach, and Structure," AIAA 2007-4296, June, 2007.
5. http://www.apg.jaxa.jp/info/event/001.html#hld-cfd.
6. NASA AST/IWD/High Lift - Trapezoidal Wing Model Archive Web Site. (http://db-www.larc.nasa.gov/trapwing/archive/).
7. Johnson. P.L., Jones K.M., Madson M.D., "Experimental Investigation of a Simplified 3D High Lift Configuration in support of CFD Validation" AIAA Paper 2000-4217, August 2000.
8. Streett. C.L., Casper. J.H., Lockard. D.P., Khorrami M.D., Stoker R.W., Elkoby R., Wenneman W.F., Under brink. J.R., "Aerodynamic Noise Reduction For High-Lift Devices on a Swept Wing Model," AIAA Paper 2006-21, January 2006.
9. Rumsey C.L. and Ying S.X., "Prediction of high-lift: Review of present CFD capability," Progress in Aerospace Sciences Vol.38 No.2 pp.145-180 2002.
10. Cummings M.R., Forsythe J.R., Morton S.A., Squires K.D., "Computational challenges in high angle of attack flow prediction," Progress in Aerospace Sciences, Vol.39, pp.369-384, 2003.
11. Nash S.M., Rogers S.E., "Numerical Study of a Trapezoidal Wing High-Lift Configuration," AIAA Paper 01-5559, October 1999.
12. Rogers S.E., Roth K., Nash S.M., "CFD Validation of High-Lift Flows With Significant Wind-Tunnel Effects," AIAA Paper 4218, Auguest 2000.
13. th AIAA Applied Aerodynamics Conference, AIAA Paper 2002-2804, June 2002.
14. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 2008.
15. Chen, S. and Doolen, G., "Lattice Boltzmann Method for Fluid Flows," Ann. Rev. Fluid Mech., Vol. 30, 1997, pp. 329-364.
16. Chapman, P. and Cowling, T., The Mathematical Theory of Non-uniform Gases, Cambridge University Press, 1990.
17. Chen, H., Teixeira, C., and Molvig, K., "Digital Physics Approach to Computational Fluid Dynamics: Some Basic Theoretical Features," Int. J. Mod. Phys. C, Vol. 8, 1997, pp. 675-684.
18. Chen, H., Chen, S. and Matthaeus, W., "Recovery of the Navier-Stokes Equations Using a Lattice-gas Boltzmann Method," Phys. Rev. A, Vol. 45, 1992, pp. 5339-5342.
19. Li, Y., Shock, R., Zhang, R. and Chen, H., "Numerical Study of Flow Past an Impulsively Started Cylinder by Lattice Blotzmann Method," J. Fluid Mech., Vol. 519, 2004, pp. 273-300.
20. Li, Y., Shock, R., Zhang, R. and Chen, H., "Simulation of Flow over Iced Airfoil by Using a Lattice Boltzmann Method," AIAA Paper 2005-1103, 43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13 2005, Reno, Nevada.
21. th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2008-34.
22. th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2008-549.
23. th AIAA/CEAS Aero acoustics Conference, AIAA Paper 2008.
24. th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2008-749.
25. Qian, Y., d'Humieres, D. and Lallemand, P., "Lattice BGK Models for the Navier-Stokes Equation," Europhys. Lett., Vol. 17, 1992, pp. 479-484.
26. Bhatnagar, P., Gross, E. and Krook, M., "A Model for Collision Processes in Gases. I. Small Amplitude Processes in Charged and Neutral One-component System," Phys. Rev., Vol. 94, 1954, pp. 511-525.
27. Chen, H., Kandasamy, S., Orszag, S., Shock, R., Succi, S., and Yakhot, V., "Extended Boltzmann Kinetic Equation for Turbulent Flows," Science, Vol. 301, 2003, pp. 633-636.
28. Yakhot, V., Chen, H. A., Staroselsky, I., Qian, Y., Shock, R., Kandasamy, S., Zhang, R., Mallick, S., and Alexander, C., "A New Approach to Modelling Strongly Non-Equilibrium, Time-Dependent Turbulent Flow," Exa internal publication, 2001.
29. Yakhot, V. and Orszag, S. A., "Renormalization Group Analysis of Turbulence. I. Basic Theory," J. Sci. Comput., Vol 1, No. 2, 1986, pp. 3-51.
30. Chen, H., "Volumetric Formulation of the Lattice Boltzmann Method for Fluid Dynamics: Basic Concept," Phys. Rev. E, Vol.58, 1998, pp.3955-3963.
31. Chen, H., Teixeira, C., and Molvig, K., "Realization of Fluid Boundary Conditions via Discrete Boltzmann Dynamics," Int. J. Mod. Phys. C, Vol. 9, 1998, pp. 1281-1292.
32. Texeira, C., "Incorporating Turbulence Models into the Lattice-Boltzmann Method," Int. J. Mod Phys. C, Vol. 9, No. 8, 1998, pp.1159-1175.
33. th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2007-127.
34. th AIAA Fluid Dynamics Conference and Exhibit, June 2005.
35. Durbin P.A.," On the k-epsilon stagnation point anomaly", International Journal of Heat and Fluid Flow, Volume 17, Number 1, February 1996, pp. 89-90(2).
36. Jeong, J and Hussain, F., 1995, "On the Identification of a Vortex," Journal of Fluid Mechanics, Vol. 285, pp. 69-94.