Effects of interface combustion and mixing on shock-tunnel conditions
- 1 September 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (9) , 1669-1671
- https://doi.org/10.2514/3.2649
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Experimental Investigation of the Equilibrium Interface TechniquePhysics of Fluids, 1962
- SURVEY OF HYPERVELOCITY IMPACT INFORMATIONPublished by Defense Technical Information Center (DTIC) ,1961
- Equation of State for Nineteen Metallic Elements from Shock-Wave Measurements to Two MegabarsJournal of Applied Physics, 1960
- The Tailored-Interface Hypersonic Shock TunnelJournal of the Aerospace Sciences, 1959