A study of unsteady fields near leading-edge slats
- 12 May 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Emendation of the Brown & Michael equation, with application to sound generation by vortex motion near a half-planeJournal of Fluid Mechanics, 1996
- Numerical Solution of Integral EquationsPublished by Springer Nature ,1990
- Effect of Leading-Edge Separation on the Lift of a Delta WingJournal of the Aeronautical Sciences, 1954