Prediction of Delta Wing Leading-Edge Vortex Circulation and Lift-Curve Slope
- 1 May 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 34 (3) , 450-452
- https://doi.org/10.2514/2.2193
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Accurate development of leading-edge vortex using an embedded conical gridAIAA Journal, 1996
- Compressible inviscid vortex flow of a sharp edge delta wingAIAA Journal, 1995
- Measurements of circulation and vorticity in the leading-edge vortexof a delta wingAIAA Journal, 1993
- Connection between leading-edge sweep, vortex lift, and vortex strength for delta wingsJournal of Aircraft, 1990
- Use of the updated NASA Langley radio-controlled drop-model technique for high-alpha studies of the X-29A configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Analytical Prediction of Vortex LiftJournal of Aircraft, 1981