Interference heating due to shock wave impingement on laminar boundary layers

This publication has 4 references indexed in Scilit:

• Experimental studies of separated flows at hypersonic speeds. II - Two-dimensional wedge separated flow studies.
  AIAA Journal, 1966
• INVESTIGATION OF HYPERSONIC INLET SHOCK-WAVE BOUNDARY LAYER INTERACTION. PART 2. CONTINUOUS FLOW TEST AND ANALYSES
  Published by Defense Technical Information Center (DTIC) ,1966
• MACH 8 TO 22 STUDIES OF FLOW SEPARATIONS DUE TO DEFLECTED CONTROL SURFACES
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1963
• Investigation of Separation and Associated Heat Transfer and Pressure Distribution on Cone-Cylinder-Flare Configurations at Mach Five
  ARS Journal, 1962