Finite-volume Euler and Navier-Stokes solvers for three-dimensional and conical vortex flows over delta wings
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Navier-Stokes computations of vortical flows over low aspect ratio wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- An implicit flux-difference splitting scheme for three-dimensional, incompressible Navier-Stokes solutions to leading edge vortex flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Influence of numerical dissipation in computing supersonic vortex-dominated flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Numerical issues in computing inviscid supersonic flow over conical delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Comparison of computations and experimental data for leading edge vortices - Effects of yaw and vortex flapsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Numerical Simulation of Tip Vortices of Wings in Subsonic and Transonic Flows,Published by Defense Technical Information Center (DTIC) ,1986
- Three-dimensional solutions to the Euler equations with one million grid pointsAIAA Journal, 1985
- Total pressure loss in vortical solutions of the conical Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A comparison of Euler and Navier-Stokes solutions for supersonic flow over a conical delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Free vortex flows - Recent encounters with an Euler codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984