Shock wave-turbulent boundary layer interaction in hypersonic flow
Author:
Affiliation:
1. Cornell Aeronautical Laboratory, Inc., Buffalo, N.Y.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-74
Reference107 articles.
1. Korkegi, Robert H. , Viscous Interactions and Flight at High Mach Numbers, AIAA Pape 1· No. 70-781
2. REFLECTION AT A LAMINAR BOUNDARY LAYER OF A WEAK STEADY DISTURBANCE TO A SUPERSONIC STREAM, NEGLECTING VISCOSITY AND HEAT CONDUCTION
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