Multi-dimensional formulation of CSCM - An upwind flux difference eigenvector split method for the compressible Navier-Stokes equations
- 13 July 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- A natural conservative flux difference splitting for the hyperbolic systems of gasdynamicsPublished by Springer Nature ,2008
- Discretization of boundary conditions on moving discontinuitiesPublished by Springer Nature ,2008
- The use of the Riemann problem in finite difference schemesPublished by Springer Nature ,1989
- Euler equations - Implicit schemes and boundary conditionsAIAA Journal, 1983
- Numerical experiments with the split-flux-vector form of the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A characteristic flux difference splitting for the hyperbolic conservation laws of inviscid gasdynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Conservative supra-characteristics method for splitting the hyperbolic systems of gasdynamics with computed boundaries for real and perfect gasesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Two-Dimensional Inlet Simulation Using a Diagonal Implicit AlgorithmAIAA Journal, 1981
- SUBJECT INDEX 1974AIAA Journal, 1974
- Computation of Steady Nozzle Flow by a Time-Dependent MethodAIAA Journal, 1974