A Method for Location of Detached Shock Waves Ahead of Plane Bodies
- 1 January 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (1) , 61-62
- https://doi.org/10.2514/8.2527
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A Second-Order Solution for an Oscillating Two-Dimensional Supersonic AirfoilJournal of the Aeronautical Sciences, 1952