Effect of Wave Interactions on Pressure Distributions in Supersonic and Hypersonic Flow
- 1 March 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (3) , 634-639
- https://doi.org/10.2514/3.54848
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- An Analytic Extension of the Shock-Expansion MethodJournal of the Aerospace Sciences, 1961
- XVIII. The flow behind a stationary shockJournal of Computers in Education, 1949