On the separation of a supersonic flow at a sharp corner.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6) , 1086-1088
- https://doi.org/10.2514/3.4141
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- Turbulent Shear Layer Re-Attachment with Special Emphasis on the Base Pressure ProblemAeronautical Quarterly, 1964