Numerical simulation of leading-edge vortex flows
- 25 June 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edgesPublished by Iowa State University ,2018
- Vortex-Lattice Method for the Calculation of the Nonsteady Separated Flow over Delta WingsJournal of Aircraft, 1981
- Euler solutions for wing and wing-body combination at supersonic speeds with leading-edge separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Leeside Flowfield and Heat Transfer of a Delta Wing at IM = POAIAA Journal, 1978
- The Estimation of the Non-Linear Lift of Delta Wings at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1963
- Effect of Leading-Edge Separation on the Lift of a Delta WingJournal of the Aeronautical Sciences, 1954