Shock-wave reflection from a turbulent boundary layer with mass bleed.

• 1 September 1968
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
• Vol. 5  (5) , 461-467
• https://doi.org/10.2514/3.43967

Abstract

Keywords

• SHOCK WAVE
• MASS BLEED
• TURBULENT BOUNDARY
• WAVE REFLECTION
• BOUNDARY LAYER