Influence of Shock-Wave Attenuation by Boundary-Layer Growth on Contact-Surface Motion in a Shock Tube
- 1 June 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (6) , 388-389
- https://doi.org/10.2514/8.8098
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A Theoretical and Experimental Study of Shock-Tube FlowsJournal of the Aeronautical Sciences, 1955