A Method for Improving the Performance of Shock Tubes
- 1 November 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 27 (11), 1191-1193
- https://doi.org/10.2514/8.12496
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Heat Transfer to Satellite Vehicles Re-entering the AtmosphereJournal of Jet Propulsion, 1957
- Tecnical NotesJournal of Jet Propulsion, 1956
- The Application of the Shock Tube to the Study of the Problems of Hypersonic FlightJournal of Jet Propulsion, 1956
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 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