Hypersonic Shock Tunnel
- 1 May 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 29 (5) , 332-340
- https://doi.org/10.2514/8.4763
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Resistance Thermometer for Transient High-Temperature StudiesJournal of Applied Physics, 1956
- A Theoretical and Experimental Study of Shock-Tube FlowsJournal of the Aeronautical Sciences, 1955
- A Method for Generating Strong Shock WavesJournal of Applied Physics, 1954
- The Production of High Temperature Gases in Shock TubesJournal of Applied Physics, 1952
- Interaction of Shock WavesReviews of Modern Physics, 1949