Aircraft computations using multigrid and an unstructured parallel library
This paper examines the application of unstructured multigrid, using a sequence of independent tetrahedral grids. The test cases examined are for inviscid flow over an aircraft and an M6 wing. The sensitivity of the method to grid sequence and cycling strategy are investigated. All of the calculat...
Main Authors: | , |
---|---|
Format: | Report |
Published: |
Unspecified
1995
|