Flow visualization model of the leeside flows over conically cambered delta wings at supersonic speeds
- 17 August 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Comparison of computations and experimental data for leading edge vortices - Effects of yaw and vortex flapsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Numerical simulation of leading-edge vortex flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964