Computation of Inviscid Flow Over Blunt Bodies Having Large Embedded Subsonic Regions
- 1 October 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (10) , 839-844
- https://doi.org/10.2514/3.61566
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Calculation of inviscid supersonic flow over ablated nosetipsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Time-Split Finite-Volume Method for Three-Dimensional Blunt-Body FlowAIAA Journal, 1973
- Computation of Three Dimentional Flows about aircraft configurationsComputers & Fluids, 1973
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Three-Dimensional Flow around Blunt BodiesAIAA Journal, 1967