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
1 The Laplace grid points become finite element mesh nodal points arranged as triangles filling space
2 All the action (triangles) is near near wing boundary
3 Use domain decomposition but no longer equal area as equal triangle count
in Table To:

© Northeast Parallel Architectures Center, Syracuse University, npac@npac.syr.edu

If you have any comments about this server, send e-mail to webmaster@npac.syr.edu.

Page produced by wwwfoil on Thu Mar 16 2000