Effect of vortices on delta wing lee-side heating at Mach 6
- 1 March 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (3) , 599-600
- https://doi.org/10.2514/3.5725
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.AIAA Journal, 1968
- Investigation of the leeward side of a delta wing at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Mixing and reaction of hydrazine and nitrogen tetroxide at elevated pressure.AIAA Journal, 1967