Calculation of vortex breakdown locations for flow over delta wings
- 1 October 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (10) , 1020-1022
- https://doi.org/10.2514/3.44635
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Reflection-Plane Tests of Spoilers on an Advanced Technology WingPublished by SAE International ,1976
- A three-dimensional solution of flows over wings with leading-edge vortex separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Vortex development and breakdownPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Spoilers for roll control of light airplanesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- FLIGHT TEST RESULTS FOR AN ADVANCED TECHNOLOGY LIGHT AIRPLANE WINGPublished by SAE International ,1974
- Vortex BreakdownAnnual Review of Fluid Mechanics, 1972