Lee-surface vortex effects over configurations in hypersonic flow
- 17 January 1972
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Hypersonic lee-surface heating alleviation on delta wing by apex-droopingAIAA Journal, 1971
- Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flowAIAA Journal, 1971
- Effect of vortices on delta wing lee-side heating at Mach 6AIAA Journal, 1970
- Predictions of vortex-lift characteristics based on a leading-edge suction analogyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.AIAA Journal, 1968
- Exact and Approximate Solutions for the Supersonic Delta WingJournal of the Aeronautical Sciences, 1956