Shock Fitting Method for Complicated Two-Dimensional Supersonic Flows
- 1 May 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (5) , 583-588
- https://doi.org/10.2514/3.61399
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Supersonic Flow and Shock WavesPublished by Springer Nature ,1976
- Conservation equations of gasdynamics in curvilinear coordinate systemsJournal of Computational Physics, 1974
- Three-dimensional, supersonic, steady flows with any number of imbedded shocksPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Computation of Three Dimentional Flows about aircraft configurationsComputers & Fluids, 1973
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969