The Generalized Shock-Expansion Method and Its Application to Bodies Traveling at High Supersonic Air Speeds
- 1 April 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (4), 231-238
- https://doi.org/10.2514/8.3316
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- On the Flow Behind an Attached Curved ShockJournal of the Aeronautical Sciences, 1952
- On Weak Interaction of Strong Shock and Mach Waves Generated Downstream of the ShockJournal of the Aeronautical Sciences, 1952
- Surface-Pressure Gradient and Shock-Front Curvature at the Edge of a Plane Ogive with Attached Shock FrontJournal of the Aeronautical Sciences, 1948
- On the Air Resistance of ProjectilesProceedings of the National Academy of Sciences, 1931