Application of steady shock polars to unsteady shock wave reflections
- 1 April 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (4) , 682-684
- https://doi.org/10.2514/3.9327
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- The inverse Mach reflectionAIAA Journal, 1985
- Computation of flow around wings based on the Euler equationsJournal of Fluid Mechanics, 1984
- Shock reflection transition in three-dimensional steady flow about interfering bodiesAIAA Journal, 1983
- Generation of boundary-conforming grids around wing-body configurations using transfinite interpolationAIAA Journal, 1982
- Experiments on transition of Mach reflexionJournal of Fluid Mechanics, 1975