Leeside Flowfield and Heat Transfer of a Delta Wing at IM = PO
- 1 February 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 16 (2) , 160-165
- https://doi.org/10.2514/3.60872
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A survey of leeside flow and heat transfer on delta planform configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Lee-side vortices on delta wings at hypersonic speeds.AIAA Journal, 1972
- Effect of vortices on delta wing lee-side heating at Mach 6AIAA Journal, 1970
- Investigation of the leeward side of a delta wing at hypersonic speeds.Journal of Spacecraft and Rockets, 1969
- Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.AIAA Journal, 1968
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964