Microramps upstream of an oblique-shock/boundary-layer interaction

AIAA Journal

Volumn 48, Issue 1, 2010, Pages 104-118

  Lee, S ^a   Goettke, M K ^b   Loth, E ^a   Tinapple, J ^b   Benek, John ^b  

^a University of Illinois at Urbana Champaign   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CENTERLINES; COMPUTATIONAL STUDIES; DISPLACEMENT THICKNESS; DOWNSTREAM BOUNDARY; FLAT PLATE; LAYER INTERACTION; MEAN VELOCITY PROFILES; MICRO VORTEX GENERATORS; PRESSURE RECOVERY; PRIMARY VORTEX; REYNOLDS-AVERAGED NAVIER-STOKES; SHAPE FUNCTIONS; SHOCK INTERACTIONS; SUPERSONIC BOUNDARY LAYER; TURBULENT EDDY; VORTEX PAIR; WAVE DRAGS;

BOUNDARY LAYER FLOW; DRAG; EXPERIMENTS; FUNCTION EVALUATION; LARGE EDDY SIMULATION; PRESSURE MEASUREMENT; REYNOLDS NUMBER; VORTEX FLOW;

ATMOSPHERIC BOUNDARY LAYER;

EID: 77049090026     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.41776     Document Type: Article

References (23)

1. Loth, E., "Smart Mesoflaps for Control of Shock Boundary Layer Interactions," AIAA Paper 2000-2476, 2000.
2. Ashill, P. R., Fulker, J. L., and Hackett, K. C., "A Review of Recent Developments in Flow Control," The Aeronautical Journal, Vol.109, No.1095, May 2005, pp. 205-232.
3. Anderson, B., Tinapple, J., and Surber, L., "Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro Array Actuation," AIAA Paper 2006-3197, 2006.
4. Garnier, E., and Sagaut, P., "Large Eddy Simulation of Shock/Boundary-Layer Interaction," AIAA Journal, Vol.40, No.10, 2002, pp. 1935-1944. doi:10.2514/2.1552 (Pubitemid 35295804)
5. Ghosh, S., Choi, J., and Edwards, J., "RANS and Hybrid LES/RANS Simulations of the Effects of Micro Vortex Generators Using Immersed Boundary Methods," AIAA Paper 2008-3728, 2008.
6. Clark, G. F., "Tri-Sonic Gas-Dynamic Facility User's Manual," U.S. Air Force Wright Aeronautical Lab., TM-82-176-FIMM, Dayton, OH, Apr. 1982.
7. Lee, S., Loth, E., Wang, C., and Kim, S., "LES of Supersonic Boundary Layers μVG's," AIAA Paper 2007-3916, 2997.
8. Fureby, C., and Grinstein, F., "Monotonically Integrated Large Eddy Simulation of Free Shear Flows," AIAA Journal, Vol.37, No.5, 1999, pp. 544-556. doi:10.2514/2.772
9. Urbin, G., Knight, D., and Zheltovodov, A. A., "Compressible Large-Eddy Simulation Using Unstructured Grid: Supersonic Turbulent Boundary Layer and Compression Corner," AIAA Paper 99-0427, 1999.
10. Lund,T.,Wu, X., and Squires, K., "Generation of Turbulent In flow Data for Spatially Developing Boundary Layer Simulations," Journal of Computational Physics, Vol.140, No.2, 1998, pp. 233-258. doi:10.1006/jcph.1998. 5882 (Pubitemid 128346379)
11. Urbin, G., Knight, D., and Zheltovodov,A. A., "Large-Eddy Simulation of a Supersonic Compression Corner, Part 1," AIAA Paper 2000-0398, 2000.
12. Loth, E., Particles, Drops and Bubbles: Fluid Dynamics and Numerical Methods, Cambridge Univ. Press (to be published).
13. Kistler, A., and Chen, W., "A Fluctuating Pressure Field in a Supersonic Turbulent Boundary Layer," Journal of Fluid Mechanics,Vol. 16, 1963, pp. 41-64. doi:10.1017/S0022112063000574
14. Xu, S., and Martin, P., "Assessment of In flow Boundary Conditions for Compressible Turbulent Boundary Layers," Physics of Fluids, Vol.16, No.7, 2004, pp. 2623-2639. doi:10.1063/1.1758218 (Pubitemid 38958034)
15. Smits, A., and Dussauge, J. P., Turbulent Shear Layers in Supersonic Flow, American Inst. of Physics, New York, 1996, Chap. 2.
16. Pirozzoli, S., and Grasso, F., "Direct Numerical Simulation of Impinging Shock Wave/Turbulent Boundary Layer Interaction at M = 2:25," Physics of Fluids, Vol.18, No.6, 2006, Paper 065113. doi:10.1063/1.2216989 (Pubitemid 43984024)
17. Baldwin, B. S., and Lomax, H., "Thin Layer Approximations and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, 1978.
18. Mellor, G. L., and Gibson, D. M., "Equilibrium Turbulent Boundary Layers," Journal of Fluid Mechanics, Vol.24, 1966, pp. 225-253. doi:10.1017/S0022112066000612
19. Ganapathisubramani, B., Clemens, N. T., and Dolling, D. S., "Large-Scale Motions in a Supersonic Turbulent Boundary Layer," Journal of Fluid Mechanics, Vol.556, 2006, pp. 271-282. doi:10.1017/ S0022112006009244 (Pubitemid 43842426)
20. Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol.32, No.8, 1994, pp. 1598-1605. doi:10.2514/3.12149
21. Spalart, P. R., and Allmaras, S. R., "AOne-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 1992-0439, 1992.
22. Pitt Ford, C., and Babinsky. H., "MicroRamp Control for Oblique Shock Wave/Boundary Layer Interactions," AIAA Paper 2007-4115, 2007.
23. Barber, T. J., Mounts, J. S., and McCormick, D. C., "Boundary Layer Energization by Means of Optimized Vortex Generators," AIAA Paper 1993-0445, 1993.