Viscous flow computations using a composite grid
Author:
Affiliation:
1. National Aerospace Laboratory, Chofu, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1128
Reference3 articles.
1. Lecture Notes in Physics;Holst T. L.,1985
2. Fig.3 FDM-FEM Composite Grid Generation Procedure for a Double Airfoil Flowfield. FDM grids. FDM grids and Cartesian grid. Remove overlapped Cartesian grid. (d) Generate FEM grid in FDM-FEM boundaries. Generate FEM grid in outer region. Overall view of FDM-FEM composite grid. (g) Computed Mach contours, Mm=O. 75, a=O'. Adaptive grid. Computed Mach contours with adaptive
3. Procedure Between Two Parallel Planes.
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