The control of asymmetric vortical flows over delta wings at high angles of attack
- 14 August 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Numerical study of the effect of tangential leading edge blowing on delta wing vortical flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Control of vortical lift on delta wings by tangential leading-edge blowingJournal of Aircraft, 1988
- The control of vortical flow on a delta wing at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Leading edge vortex dynamics on a delta wing undergoing a wing rock motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Use of differential leading edge flaps for lateral control at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Dynamic load measurements with delta wings undergoing self-induced roll oscillationsJournal of Aircraft, 1984