Numerical simulation of tip vortices of wings in subsonic and transonic flows
- 12 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Euler equation analysis of the initial roll-up of aircraft wakesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Computation of the tip vortex off a low-aspect-ratio wingAIAA Journal, 1985
- Convergence acceleration for a three-dimensional Euler/Navier-Stokeszonal approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Computational-experimental pressure distributions on a transonic, low-aspect-ratio wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Computation of simple three-dimensional wing-vortex interaction in transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A diagonal form of an implicit approximate-factorization algorithmJournal of Computational Physics, 1981
- Generation of Body-Fitted Coordinates Using Hyperbolic Partial Differential EquationsSIAM Journal on Scientific and Statistical Computing, 1980
- Formation of a Trailing VortexJournal of Aircraft, 1979
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976