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Aircraft computations using multigrid and an unstructured parallel library

Abstract:

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 calculations were performed on a parallel computer. This was achieved by using the OPlus library which, by the straightforward insertion of subroutine calls, facilitates parallelisation of the resulting co...

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Publisher:
Unspecified
Publication date:
1995-10-01
UUID:
uuid:a9cafe71-6427-481c-b8a9-173454510182
Local pid:
oai:eprints.maths.ox.ac.uk:1337
Deposit date:
2011-06-12

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