Two-dimensional Euler computations on a triangular mesh using an upwind, finite-volume scheme
- 9 January 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Time-accurate Euler equations solutions on dynamic blocked gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- An unstructured multigrid method for elliptic problemsInternational Journal for Numerical Methods in Engineering, 1987
- Characteristic-Based Schemes for the Euler EquationsAnnual Review of Fluid Mechanics, 1986
- A self-adaptive-grid method with application to airfoil flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- An efficient iteration strategy for the solution of the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A 3-D chimera grid embedding techniquePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Finite volume solution of the two-dimensional Euler equations on a regular triangular meshPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A comparison of finite volume flux vector splittings for the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- On a Class of High Resolution Total-Variation-Stable Finite-Difference SchemesSIAM Journal on Numerical Analysis, 1984
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981