Three-dimensional supersonic internal flows
- 14 July 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Mach Reflection Associated with Over-Expanded Nozzle Free Jet FlowsAIAA Journal, 1975
- Mach Disk from Underexpanded Axisymmetric Nozzle FlowAIAA Journal, 1974
- On the shock-on-shock interaction problemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- BOUNDARY CONDITION CALCULATION PROCEDURES FOR INVISCID SUPERSONIC FLOW FIELDS*Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- A Method for the Numerical Calculation of Hydrodynamic ShocksJournal of Applied Physics, 1950