Upstream influence of the base pressure.
- 1 March 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (3) , 466-471
- https://doi.org/10.2514/3.4521
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A new theoretical solution of the laminar, hypersonic near wake.AIAA Journal, 1967
- 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