Spatial adaptation procedures on tetrahedral meshes for unsteady aerodynamic flow calculations
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- A compact higher order Euler solver for unstructured grids with curved boundariesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Accuracy of an unstructured-grid upwind-Euler algorithm for the ONERA M6 wingJournal of Aircraft, 1991
- Spatial adaption procedures on unstructured meshes for accurate unsteady aerodynamic flow computationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Three-dimensional flux-split Euler schemes involving unstructured dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Euler flutter analysis of airfoils using unstructured dynamic meshesJournal of Aircraft, 1990
- Adaptive H-refinement on 3-D unstructured grids for transient problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Finite elements in CFD: What lies aheadInternational Journal for Numerical Methods in Engineering, 1987
- Self-adaptive-grid method with application to airfoil flowAIAA Journal, 1987
- Grid adaptation for the 2-D Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A survey of dynamically-adaptive grids in the numerical solution of partial differential equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984