Microramp control of supersonic oblique shock-wave/boundary-layer interactions

AIAA Journal

Volumn 47, Issue 3, 2009, Pages 668-675

  Babinsky, H ^a,b   Li, Y ^a,b   Ford, C W Pitt ^a,b  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b Department of Engineering ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ADVERSE PRESSURE GRADIENTS; BOUNDARY-LAYER; BREAK-UP; DELAY SEPARATIONS; ENGINE INLETS; FLOW FEATURES; LAYER INTERACTIONS; PERFORMANCE INDICATORS; REFLECTED SHOCKS; SEPARATED REGIONS; VORTEX GENERATORS; VORTICAL FLOWS;

BOUNDARY LAYER FLOW; INTAKE SYSTEMS;

BOUNDARY LAYERS;

EID: 62149091794     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.38022     Document Type: Article

References (8)

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3. McCormick, D. C., "Shock/Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity," AIAA Journal, Vol. 31, No. 1, Jan. 1993, pp. 91-96. doi: 10.2514/3.11323
4. Holden, H. A., Babinsky, H., "Effect of Microvortex Generators on Separated Normal Shock/Boundary Layer Interactions," Journal of Aircraft, Vol. 44, No. 1, Jan.-Feb. 2007, pp. 170-174. doi:10.2514/1.22770
5. Lin, J. C., "Review of Research on Low-Profile Vortex Generators to Control Boundary-Layer Separation," Progress in Aerospace Sciences, 2002.
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7. Anderson, B., Tinapple, J., and Surber, L., "Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation," AIAA Fluids Engineering Conference, San Francisco, AIAA Paper 2006-3197, June 2006.
8. Sun, C. C., and Childs, M. E., "A Modified Wall Wake Velocity Profile for Turbulent Compressible Boundary Layers," Journal of Aircraft, Vol. 10, 1973, pp. 381-383. doi: 10.2514/3.44376