Computational efficiency achieved by time splitting of finite difference operators
- 17 January 1972
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Difference methods for hyperbolic equations using space and time split difference operators of third order accuracyPublished by Springer Nature ,2008
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- A systematic development of the supersonic flow fields over and behind wings and wing-body configurations using a shock-capturing finite-difference approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Time-dependent computation of transonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- NUMERICAL ADVECTION EXPERIMENTS1Monthly Weather Review, 1968