Numerical solution of the Euler equations for complex aerodynamic configurations using an edge-based finite element scheme
- 6 July 1993
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Adaptive edge-based finite element schemes for the Euler and Navier-Stokes equations on unstructured gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- A 3D finite element multigrid solver for the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Implicit solvers for unstructured meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Numerical aspects of computing high Reynolds number flows on unstructured meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- 2-D and 3-D Euler computations with finite element methods in aerodynamicsPublished by Springer Nature ,1987
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order schemeJournal of Computational Physics, 1974