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Parallel computing strategies for block multigrid implicit solution of the Euler equationsA multigrid diagonal implicit algorithm has been developed to solve the three-dimensional Euler equations of inviscid compressible flow on block-structured grids. An improved method of advancing the multigrid cycle has been examined with respect to convergence rates, accuracy, and efficiency. In this method, the multigrid cycle is advanced independently in each of the blocks, and the information exchange between the blocks is done using buffer arrays, allowing for the asynchronous updating of interface boundary conditions. This updating scheme is used to eliminate the convergence problems found in a previous implementation of the algorithm while retaining its potential for efficient parallel execution. Results are computed for transonic flows past wings and include pressure distributions to verify the accuracy of the scheme and convergence histories to demonstrate the efficiency of the method. Efficiencies that were obtained using a modest number of processors in parallel are also presented and discussed.
Document ID
19920064270
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Yadlin, Yoram
(NASA Ames Research Center Moffett Field, CA, United States)
Caughey, David A.
(Cornell University Ithaca, NY, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Publication Information
Publication: AIAA Journal
Volume: 30
Issue: 8 Au
ISSN: 0001-1452
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0001-1452
Accession Number
92A46894
Funding Number(s)
CONTRACT_GRANT: NAG2-665
Distribution Limits
Public
Copyright
Other

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