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A Framework for Parallel Unstructured Grid Generation for Complex Aerodynamic SimulationsA framework for parallel unstructured grid generation targeting both shared memory multi-processors and distributed memory architectures is presented. The two fundamental building-blocks of the framework consist of: (1) the Advancing-Partition (AP) method used for domain decomposition and (2) the Advancing Front (AF) method used for mesh generation. Starting from the surface mesh of the computational domain, the AP method is applied recursively to generate a set of sub-domains. Next, the sub-domains are meshed in parallel using the AF method. The recursive nature of domain decomposition naturally maps to a divide-and-conquer algorithm which exhibits inherent parallelism. For the parallel implementation, the Master/Worker pattern is employed to dynamically balance the varying workloads of each task on the set of available CPUs. Performance results by this approach are presented and discussed in detail as well as future work and improvements.
Document ID
20090007630
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Zagaris, George
(College of William and Mary Williamsburg, VA, United States)
Pirzadeh, Shahyar Z.
(NASA Langley Research Center Hampton, VA, United States)
Chrisochoides, Nikos
(College of William and Mary Williamsburg, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 5, 2009
Subject Category
Mathematical And Computer Sciences (General)
Report/Patent Number
LF99-7128
Meeting Information
Meeting: 47th AIAA Aerospace Sciences Meeting and Exhibit
Location: Orlando, FL
Country: United States
Start Date: January 5, 2009
End Date: January 8, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.07.20.02
CONTRACT_GRANT: NNX07AM10H
CONTRACT_GRANT: NNL06AA02H
Distribution Limits
Public
Copyright
Public Use Permitted.
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