Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes
- 1 November 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (11) , 1836-1843
- https://doi.org/10.2514/3.10808
Abstract
No abstract availableKeywords
This publication has 17 references indexed in Scilit:
- Finite element Euler computations in three dimensionsInternational Journal for Numerical Methods in Engineering, 1988
- Multigrid solution of the two-dimensional Euler equations on unstructured triangular meshesAIAA Journal, 1988
- A point implicit unstructured grid solver for the Euler and Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Some useful data structures for the generation of unstructured gridsCommunications in Applied Numerical Methods, 1988
- Finite elements in CFD: What lies aheadInternational Journal for Numerical Methods in Engineering, 1987
- Comparison of finite volume flux vector splittings for the Euler equationsAIAA Journal, 1986
- Finite volume solution of the two-dimensional Euler equations on a regular triangular meshAIAA Journal, 1986
- Calculation of Inviscid Transonic Flow over a Complete AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Flux-vector splitting for the Euler equationsPublished by Springer Nature ,1982
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981