Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Experimental study of shock wave interference heating on a cylindrical leading edge at Mach 6 and 8Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A review of aerothermal problems associated with hypersonic flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.Published by Office of Scientific and Technical Information (OSTI) ,1968
- Laminar Heat Transfer Around Blunt Bodies in Dissociated AirJournal of the Aerospace Sciences, 1959