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Parallelization of an Object-Oriented Unstructured Aeroacoustics SolverA computational aeroacoustics code based on the discontinuous Galerkin method is ported to several parallel platforms using MPI. The discontinuous Galerkin method is a compact high-order method that retains its accuracy and robustness on non-smooth unstructured meshes. In its semi-discrete form, the discontinuous Galerkin method can be combined with explicit time marching methods making it well suited to time accurate computations. The compact nature of the discontinuous Galerkin method also makes it well suited for distributed memory parallel platforms. The original serial code was written using an object-oriented approach and was previously optimized for cache-based machines. The port to parallel platforms was achieved simply by treating partition boundaries as a type of boundary condition. Code modifications were minimal because boundary conditions were abstractions in the original program. Scalability results are presented for the SCI Origin, IBM SP2, and clusters of SGI and Sun workstations. Slightly superlinear speedup is achieved on a fixed-size problem on the Origin, due to cache effects.
Document ID
19990028612
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Baggag, Abdelkader
(Purdue Univ. West Lafayette, IN United States)
Atkins, Harold
(NASA Langley Research Center Hampton, VA United States)
Oezturan, Can
(Bogazici Univ. Istanbul, Turkey)
Keyes, David
(Institute for Computer Applications in Science and Engineering Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1999
Subject Category
Computer Programming And Software
Report/Patent Number
ICASE-99-11
NAS 1.26:209098
NASA/CR-1999-209098
Report Number: ICASE-99-11
Report Number: NAS 1.26:209098
Report Number: NASA/CR-1999-209098
Funding Number(s)
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-97046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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