Predictions of vortex-lift characteristics based on a leading-edge suction analogy
- 16 August 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The Estimation of the Non-Linear Lift of Delta Wings at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1963