A supersonic maneuver wing designed for nonlinear attached flow
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Supersonic nonlinear potential flow with subsonic regions and implicit isentropic shock fittingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Controlled supercritical crossflow on supersonic wings - An experimental validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- The nonlinear supersonic potential flow over delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Opportunities for supersonic performance gains through non-linear aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A numerical procedure for the computation of supersonic conical flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978