Hypersonic Boundary-Layer Transition

This publication has 22 references indexed in Scilit:

• On nonlinear aspects of hypersonic boundary-layer stability
  AIAA Journal, 1988
• Mach 6 Experiments of Transition on a Cone at Angle of Attack
  Journal of Spacecraft and Rockets, 1982
• Effects of Wind Tunnel Disturbances on Boundary-Layer Transition with Emphasis on Radiated Noise: A Review
  Published by Defense Technical Information Center (DTIC) ,1980
• Boundary-Layer Stability and Transition
  Annual Review of Fluid Mechanics, 1976
• Development of a High Reynolds Number Quiet Tunnel for Transition Research
  AIAA Journal, 1975
• Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
  AIAA Journal, 1975
• Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
  AIAA Journal, 1975
• An Implicit Method for Three-Dimensional Viscous Flow with Application to Cones at Angle of Attack
  Published by Defense Technical Information Center (DTIC) ,1973
• Shock tunnel investigation of boundary-layer transition at M equals 5.5.
  AIAA Journal, 1967
• EFFECTS OF NOSE BLUNTNESS ON THE BOUNDARY LAYER CHARACTERISTICS OF CONICAL BODIES AT HYPERSONIC SPEEDS
  Published by Defense Technical Information Center (DTIC) ,1966