A Contribution to the Numerical Prediction of Unsteady Flows
- 1 May 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (5) , 602-610
- https://doi.org/10.2514/3.48491
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
- The use of the Riemann problem in finite difference schemesPublished by Springer Nature ,1989
- Numerical experiments with the Osher upwind scheme for the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Upwind difference schemes for hyperbolic systems of conservation lawsMathematics of Computation, 1982
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- Numerical experiments on the leading edge flow fieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- Shock fitting for everybodyComputers & Fluids, 1980
- The λ-schemeComputers & Fluids, 1979
- Towards the ultimate conservative difference scheme. IV. A new approach to numerical convectionJournal of Computational Physics, 1977