Influence of numerical dissipation in computing supersonic vortex-dominated flows
- 12 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- 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
- Total pressure loss in vortical solutions of the conical Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A nonlinear hybrid vortex method for wings at large angle of attackAIAA Journal, 1984
- Thermal conductivity of partially ionized hydrogenFluid Dynamics, 1978