A two-dimensional, TVD numerical scheme for inviscid, high Mach number flows in chemical equilibrium
- 2 June 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Three-dimensional AOTV flowfields in chemical nonequilibriumPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A shock capturing technique for hypersonic, chemically relaxing flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- CAG12 - A CSCM based procedure for flow of an equilibrium chemicallyreacting gasPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- AOTV Bluff Body Flow-Relaxation AlgorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Numerical solution of Space Shuttle Orbiter flow field including real gas effectsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Forebody and base region real-gas flow in severe planetary entry by a factored implicit numerical method. I - Computational fluid dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Diffraction of a Shock Wave by a Compression Corner: Part II - Single Mach ReflectionAIAA Journal, 1978