Pressure induced by weak interaction with unsteady hypersonic boundary layers.
- 1 August 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (8) , 1609-1610
- https://doi.org/10.2514/3.5443
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 1953