Computation of shock wave reflection by circular cylinders
- 1 May 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (5) , 683-689
- https://doi.org/10.2514/3.9683
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Analytical prediction of the transition from Mach to regular reflection over cylindrical concave wedgesJournal of Fluid Mechanics, 1985
- A numerical study of oblique shock-wave reflections with experimental comparisonsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1985
- Numerical solution of the two-dimensional Euler equations by second-order upwind difference schemesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The numerical simulation of two-dimensional fluid flow with strong shocksJournal of Computational Physics, 1984
- High resolution schemes for hyperbolic conservation lawsJournal of Computational Physics, 1983
- A characteristic flux difference splitting for the hyperbolic conservation laws of inviscid gasdynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Flux-vector splitting for the Euler equationsPublished by Springer Nature ,1982
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- Diffraction of strong shocks by cones, cylinders, and spheresJournal of Fluid Mechanics, 1961
- A new approach to problems of shock dynamics Part I Two-dimensional problemsJournal of Fluid Mechanics, 1957