Rapid expansion of a supersonic boundary layer and its application to the near wake.
- 1 February 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (2) , 217-226
- https://doi.org/10.2514/3.3422
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Laminar, transitional, and turbulent heat transfer after a sharp convex cornerAIAA Journal, 1964
- Effect of Wave Interactions on Pressure Distributions in Supersonic and Hypersonic FlowAIAA Journal, 1963
- On the Air Resistance of ProjectilesProceedings of the National Academy of Sciences, 1931