Spatial adaptation of unstructured meshes for unsteady aerodynamic flow computations
- 1 May 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (5) , 1243-1251
- https://doi.org/10.2514/3.11057
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Euler flutter analysis of airfoils using unstructured dynamic meshesJournal of Aircraft, 1990
- Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Numerical simulation of shock-elevated box interaction using an adaptive finite element shock capturing schemePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Adaptive H-refinement on 3-D unstructured grids for transient problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- An adaptive finite element solver for transient problems with moving bodiesComputers & Structures, 1988
- Adaptive remeshing for compressible flow computationsJournal of Computational Physics, 1987
- Self-adaptive-grid method with application to airfoil flowAIAA Journal, 1987
- An adaptive finite element method for high speed flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Improved adaptive refinement strategies for finite element aerodynamic computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A survey of dynamically-adaptive grids in the numerical solution of partial differential equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984