Second- and Third-Order Noncentered Difference Schemes for Nonlinear Hyperbolic Equations
- 1 February 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (2) , 189-196
- https://doi.org/10.2514/3.50449
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- A complete numerical technique for the calculation of three-dimensional inviscid supersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971
- Third order difference methods for hyperbolic equationsJournal of Computational Physics, 1970
- On difference schemes of third order accuracy for nonlinear hyperbolic systemsJournal of Computational Physics, 1970
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Heuristic stability theory for finite-difference equationsJournal of Computational Physics, 1968
- Runge-Kutta methods with minimum error boundsMathematics of Computation, 1962
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954