LU-SGS implicit scheme for entry vehicle flow computation and comparison with aerodynamic data
- 22 June 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- An implicit three-dimensional Navier-Stokes solver for compressible flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Nonequilibrium thermo-chemical calculations using a diagonal implicit schemePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Characteristic-based algorithms for flows in thermo-chemical nonequilibriumPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Efficient real gas Navier-Stokes computations of high speed flows using an LU schemePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Lower-upper implicit schemes with multiple grids for the Euler equationsAIAA Journal, 1987
- Uniformly High-Order Accurate Nonoscillatory Schemes. ISIAM Journal on Numerical Analysis, 1987
- Comparison of finite volume flux vector splittings for the Euler equationsAIAA Journal, 1986
- 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
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980