A new, improved computational technique for two-dimensional, unsteady, compressible flows
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Difference methods for initial-boundary-value problems and computation of flow around bodiesComputers & Fluids, 1981
- Unsteady compressible flow - A computational method consistent with the physical phenomenaAIAA Journal, 1981
- Numerical experiments on the leading edge flow fieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Critical study of calculations of subsonic flows in ductsAIAA Journal, 1981
- Upwind Second-Order Difference Schemes and Applications in Aerodynamic FlowsAIAA Journal, 1976