Trailing edge flap influence on leading edge vortex flap aerodynamics
- 1 February 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (2) , 165-169
- https://doi.org/10.2514/3.44846
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Effects of yaw on leading edge vortex flap aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- The aerodynamics of inverted leading edge flaps on delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Modern fluid dynamics of subsonic and transonic flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980