A normal shock-wave turbulent boundary-layer interaction at transonic speeds
- 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:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Flowfield Measurements Using a Total Temperature Probe at Hypersonic SpeedsAIAA Journal, 1972
- Behavior of turbulent flow near a porous wall with pressure gradientAIAA Journal, 1970