A supersonic maneuver wing designed for nonlinear attached flow
Author:
Affiliation:
1. Grumman Aerospace Corp., Bethpage, NY
2. NASA, Langley Research Center, High Speed Aerodynamics Div., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-425
Reference14 articles.
1. Opportunities for supersonic performance gains through non-linear aerodynamics
2. Mason, W.H.; and Miller, D.S. "Controlled Supercritical Crossflow on Supersonic Wings - An Experimental Validation," AIAA Paper No. 80-1421, July 1980.
3. A numerical procedure for the computation of supersonic conical flows
4. The nonlinear supersonic potential flow over delta wings
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