Basic HTML version of Foils prepared 13 February 2000

Foil 22 Irregular 2D Simulation -- Flow over an Airfoil

From Methodology of Computational Science CPS615 Computational Science -- Spring Semester 2000. by Geoffrey C. Fox
The Laplace grid points become finite element mesh nodal points arranged as triangles filling space
All the action (triangles) is near near wing boundary
Use domain decomposition but no longer equal area as equal triangle count

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