Approximate Solutions for Supersonic Flow over Wedges and Cones
- 1 January 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (1) , 71-73
- https://doi.org/10.2514/8.8385
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A Note on the Calculation of Oblique Shock-Wave CharacteristicsJournal of the Aeronautical Sciences, 1950