High angle-of-attack control enhancement on a forward swept wing aircraft
- 10 August 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- An experimental study of pneumatic vortex flow control on high angleof attack forebody modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992