Development of a vortex-lift-design method and application to a slender maneuver-wing configuration
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Recent advances in the solution of three-dimensional flow over wings with leading edge vortex separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Subsonic Vortex-Flow Design Study for Slender WingsJournal of Aircraft, 1978
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971