Shock wave-turbulent boundary layer interaction at a high Reynolds number, including separation and flowfield measurements
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow.AIAA Journal, 1966
- The Turbulent Boundary Layer in a Compressible FluidPhysics of Fluids, 1964
- Separation of a Supersonic Turbulent Boundary LayerJournal of the Aeronautical Sciences, 1955