A Divergent Shock Tube for Obtaining Supersonic Flows
- 1 April 1956
- journal article
- Published by Physical Society of Japan in Journal of the Physics Society Japan
- Vol. 11 (4) , 434-439
- https://doi.org/10.1143/jpsj.11.434
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Experimental Studies of Supersonic Flow past a Circular CylinderJournal of the Physics Society Japan, 1956
- A Shock Tube Method of Generating Hypersonic FlowsJournal of the Aeronautical Sciences, 1951
- Exploratory Wind-Tunnel Investigation of Wings and Bodies at M=6.9Journal of the Aeronautical Sciences, 1951
- Studies with an Aerodynamically Instrumented Shock TubeJournal of Applied Physics, 1950