Prediction of leading-edge vortex breakdown on a delta wing oscillating in roll
- 22 June 1992
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Effect of the Adverse Pressure Gradient on Vortex BreakdownAIAA Journal, 1974
- Vortex breakdown in swirling conical flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971