Simulations of mesoflap flow control for ramp oblique shock/boundary layer interactions

32nd AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Kim, S D ^a   Loth, E ^a   Dutton, J C ^b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

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

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW CONTROL;

COMPRESSION CORNERS; COMPUTATIONAL INVESTIGATION; DISPLACEMENT THICKNESS; FLOW CONTROL METHODS; MOMENTUM THICKNESS; RECIRCULATIONS; SHOCK/BOUNDARY LAYER INTERACTIONS; TOTAL PRESSURE RECOVERY;

AEROELASTICITY;

EID: 85086489849     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3117     Document Type: Conference Paper

References (10)

1. Raghunathan, S., "Passive Control of Shock Boundary Layer Interaction," Progress in Aerospace Science, Vol. 25, pp. 271-296, 1988.
2. Gefroh, D. L., "Experimental Study of Mesoflaps to Control Oblique Shock/Boundary-Layer Interaction," M. S. Thesis, University of Illinois at Urbana-Champaign, 2000.
3. Hafenrichter, E. S., Lee, Y., McIlwain, S. T., Dutton, J. C., and Loth, E., "Experiments on Normal Shock/Boundary Layer Interaction Control Using Aeroelastic Mesoflaps," 39th AIAA Aerospace Sciences Meeting, AIAA 2001- 0156, Reno, NV, 2001.
4. Bur, R., Corbel, B., and Delery, J., "Study of Passive Control in a Transonic Shock- Wave/Boundary Layer Interaction," AIAA Journal, Vol. 36, pp. 394-400, 1998.
5. McCormick, D. C., "Shock/Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity," AIAA Journal, Vol. 31, pp. 91-96, 1993.
6. Barth, T. J. and Jespersen, D., "The Design and Application of Upwind Schemes on Unstructured Meshes," 27th AIAA Aerospace Sciences Meeting, AIAA-89-0366, Reno, NV, 1989.
7. Chen, H. C. and Patel, V. C., "Near-Wall Turbulence Models for Complex Flows Including Separation," AIAA Journal, Vol. 26, pp. 641-648, 1988.
8. Kuntz, D. W., Amatucci, V. A., and Addy, A. L., "Turbulent Boundary Layer Properties Downstream of the Shock Wave/Boundary Layer Interaction," AIAA Journal, Vol. 25, pp. 668-675, 1987.
9. Settles, G. S., Fitzpatrick, T. J., and Bogdonoff, S. M., "Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow," AIAA Journal, Vol. 17, pp. 579-585, 1979.
10. Erm, L. P., Smits, A. J., and Joubert, P. N., "Low Reynolds Number Turbulent Boundary Layers on a Smooth Flat Surface in a Zero Pressure Gradient," Turbulent Shear Flow 5, pp. 186-196, 1987.