Interaction of a laminar hypersonic boundary layer and a corner expansion wave

This publication has 11 references indexed in Scilit:

• Interaction of a laminar hypersonic boundary layer and a corner expansion wave
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1969
• Rapid expansion of a supersonic boundary layer and its application to the near wake.
  AIAA Journal, 1966
• Integral Method in Compressible Laminar Boundary Layers and its Application
  Physics of Fluids, 1966
• Shock-Induced Separation of a Laminar Boundary Layer in Supersonic Flow Past a Convex Corner
  Aeronautical Quarterly, 1965
• Laminar, transitional, and turbulent heat transfer after a sharp convex corner
  AIAA Journal, 1964
• The Theory of Laminar Boundary Layers in Compressible Fluids
  Physics Today, 1964
• USE OF LOCAL SIMILARITY CONCEPTS IN HYPERSONIC VISCOUS INTERACTION PROBLEMS
  AIAA Journal, 1963
• Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds
  Journal of Jet Propulsion, 1956
• On boundary layers and upstream influence II. Supersonic flows without separation
  Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953
• A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams
  Journal of the Aeronautical Sciences, 1952