The Application of the Shock Tube to the Study of the Problems of Hypersonic Flight
- 1 July 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 26 (7) , 549-554
- https://doi.org/10.2514/8.7091
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A new shock tube technique for the study of high temperature gas phase reactionsSymposium (International) on Combustion, 1955
- Equation of State of Gases by Shock Wave Measurements. II. The Dissociation Energy of NitrogenThe Journal of Chemical Physics, 1955
- Measurement of Wall Temperature and Heat Flow in the Shock TubeJournal of Applied Physics, 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
- A Shock Tube Method of Generating Hypersonic FlowsJournal of the Aeronautical Sciences, 1951