Impact of flow unsteadiness on maneuvers and loads of agile aircraft
- 3 April 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Low speed wind tunnel investigation of the flow about delta wing, oscillating in pitch to very high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Agile Fighter Aircraft SimulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The separated flow field on a slender wing undergoing transient pitching motionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Visualization measurements of vortex flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Leading edge vortex dynamics on a pitching delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- On the feasibility of low-speed aircraft maneuvers involving extreme angles of attackJournal of Fluids and Structures, 1987
- Unsteady vortical flow around three-dimensional lifting surfacesAIAA Journal, 1986
- Optimization of Tactical Aircraft Maneuvers Utilizing High Angles of AttackJournal of Guidance, Control, and Dynamics, 1982
- Future fighter technologiesJournal of Aircraft, 1980