A Critique of Shock-Expansion Theory
- 1 October 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (10) , 673-680
- https://doi.org/10.2514/8.3433
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- TWO-DIMENSIONAL ROTATIONAL FLOW AT HIGH MACH NUMBER PAST THIN AEROFOILSThe Quarterly Journal of Mechanics and Applied Mathematics, 1952
- Two-Dimensional Airfoils in Hypersonic FlowsJournal of the Aeronautical Sciences, 1949