An implicit flux-vector splitting scheme for the computation of viscous hypersonic flow
- 9 January 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An unfactored implicit scheme with multigrid acceleration for the solution of the Navier-Stokes equationsComputers & Fluids, 1987
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's methodJournal of Computational Physics, 1979