Pneumatic vortical flow control at high angles of attack
- 8 January 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Development of non-conventional control methods for high angle of attack flight using vortex manipulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The control of vortical lift on delta wings by tangential leading edge blowingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Computation of turbulent supersonic flows around pointed bodies having crossflow separationJournal of Computational Physics, 1986
- Control of forebody vortex orientation to alleviate side forcesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980