Turbulent boundary-layer properties downstream of the shock-wave/boundary-layer interaction
- 1 May 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (5) , 668-675
- https://doi.org/10.2514/3.9681
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- The Structure of Turbulence in a Supersonic Shock-Wave/Boundary-Layer InteractionAIAA Journal, 1984
- Behavior of a turbulent boundary-layer subjected to a shock-induced separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Hot-wire investigation of an unseparated shock-wave/turbulent boundary layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Investigation of Turbulent Boundary-Layer Separation Using Laser VelocimetryAIAA Journal, 1979
- Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic FlowAIAA Journal, 1979
- Details of a Shock-Separated Turbulent Boundary Layer at a Compression CornerAIAA Journal, 1976
- Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds NumbersAIAA Journal, 1976
- Turbulence in a Shock-Wave Boundary-Layer InteractionAIAA Journal, 1975
- Biasing correction for individual realization of laser anemometer measurements in turbulent flowsPhysics of Fluids, 1973
- Mixing length and kinematic eddy viscosity in a compressible boundary layer.AIAA Journal, 1968