A Closed-Form Solution to Oblique Shock-Wave Properties
- 1 January 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (1) , 66
- https://doi.org/10.2514/3.59421
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Structure of trailing vortices.Journal of Aircraft, 1968