An implicit multigrid scheme for hypersonic strong‐interaction flowfields
- 1 September 1992
- journal article
- Published by Wiley in Communications in Applied Numerical Methods
- Vol. 8 (9) , 683-693
- https://doi.org/10.1002/cnm.1630080914
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Computational Study of Laminar Hypersonic Flow Over A 2-D RampPublished by Springer Nature ,1992
- Navier-Stokes computations of vortical flows over low-aspect-ratio wingsAIAA Journal, 1990
- Development of a multigrid code for 3-D Navier-Stokes equations and its application to a grid-refinement studyComputers & Fluids, 1990
- A validation study of four Navier-Stokes codes for high-speed flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978