Experimental investigations of the vortex flow on delta wings at high incidence
- 1 April 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (4) , 1027-1032
- https://doi.org/10.2514/3.11023
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Effect of leading edge roundness on a delta wing in wing-rock motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Suppression of vortex asymmetry behind circular conesAIAA Journal, 1990
- Suppression of asymmetry of the vortex flow behind a circular cone at high incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Similarity in Vortex Asymmetries over Slender Bodies and WingsAIAA Journal, 1977
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968