BOUNDARY CONDITION CALCULATION PROCEDURES FOR INVISCID SUPERSONIC FLOW FIELDS*
- 19 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Computational efficiency achieved by time splitting of finite difference operatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Time-dependent solutions of nonequilibrium airflow past a blunt bodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Three-dimensional flow around blunt bodies with sharp shouldersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Hypersonic flow over cones with attached and detached shock wavesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack.AIAA Journal, 1966
- On certain finite difference schemes for hyperbolic systemsMathematics of Computation, 1964