A Shock Tube Method of Generating Hypersonic Flows
- 1 December 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (12) , 803-804
- https://doi.org/10.2514/8.2124
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Studies with an Aerodynamically Instrumented Shock TubeJournal of Applied Physics, 1950
- Unsteady One-Dimensional Flows with Heat Addition or Entropy GradientsJournal of the Aeronautical Sciences, 1948
- Explosion waves and shock waves VI. The disturbance produced by bursting diaphragms with compressed airProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1946