Experimental study of high-enthalpy shock- tunnel flow. II - Nozzle-flow characteristics.
- 1 September 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (9), 1717-1724
- https://doi.org/10.2514/3.5381
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Application of microwave and optical diagnostic techniques in shock-tube and shock-tunnel flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Nonequilibrium Expansions of Air with Coupled Chemical ReactionsPhysics of Fluids, 1962
- A METHOD OF CALCULATING TURBULENT-BOUNDARY-LAYER GROWTH AT HYPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1959