The control of vortical flow on a delta wing at high angles of attack
- 17 August 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Forebody vortex management for yaw control at high angles of attackJournal of Aircraft, 1987
- Leading edge vortex dynamics on a delta wing undergoing a wing rock motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Aerodynamic aspects of aircraft dynamics at high angles of attackJournal of Aircraft, 1983
- The fluid mechanics of slender wing rockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983