Experimental studies of shock wave/wall jet interaction in hypersonic flow
- 8 January 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Film CoolingPublished by Elsevier ,1971
- Film cooling effectiveness in hypersonic turbulent flowAIAA Journal, 1970
- Turbulent boundary layer shock interaction with and without injectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970