Assessment of CFD capability for prediction of hypersonic shock interactions
- 1 January 2012
- journal article
- Published by Elsevier BV in Progress in Aerospace Sciences
- Vol. 48-49, 8-26
- https://doi.org/10.1016/j.paerosci.2011.10.001
Abstract
No abstract availableKeywords
This publication has 29 references indexed in Scilit:
- Computational Fluid Dynamics Methods for Hypersonic Flow Around Blunted-Cone-Cylinder-FlareJournal of Spacecraft and Rockets, 2010
- Transport properties of partially ionized and unmagnetized plasmasPhysical Review E, 2004
- Transport algorithms for partially ionized and unmagnetized plasmasJournal of Computational Physics, 2004
- Advances in turbulent flow computations using high-resolution methodsProgress in Aerospace Sciences, 2003
- Data-Parallel Line Relaxation Method for the Navier-Stokes EquationsAIAA Journal, 1998
- A Sequel to AUSM: AUSM+Journal of Computational Physics, 1996
- On the accuracy and efficiency of CFD methods in real gas hypersonicsInternational Journal for Numerical Methods in Fluids, 1993
- An implicit characteristic-flux-averaging method for the euler equations for real gasesInternational Journal for Numerical Methods in Fluids, 1991
- Flux-split algorithms for flows with non-equilibrium chemistry and vibrational relaxationJournal of Computational Physics, 1990
- The solution of the Navier-Stokes equations using Gauss-Seidel line relaxationComputers & Fluids, 1989