A high density, high velocity equilibrium freestream shock tunnel concept
- 22 January 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- STATUS OF RESEARCH ON MAGNETOHYDRODYNAMIC AUGMENTATION OF A SHOCK TUNNELPublished by Defense Technical Information Center (DTIC) ,1966
- Nonequilibrium effects on high-enthalpy expansions of air.AIAA Journal, 1965
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964