Abstract
We demonstrate the use of fine-grain parallel iterations in multigrid smoothers for com-putational fluid dynamics. Asynchronous iterations, incomplete sparse approximate inverses and their combinations are proposed and their effectiveness studied for a few benchmark cases of external aerodynamics. Our implementations of these solvers have focused on exploiting the wide vector units and the large number of cores on the Xeon Phi Knights Landing proces-sors. The new smoothers have been tested on some benchmark aerodynamics cases. Two of the proposed solvers, block symmetric Gauss-Seidel and asynchronous block incomplete LU factorization, both with incomplete sparse approximate inverse application, have been found to be promising.
Original language | English |
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Title of host publication | AIAA Scitech 2020 Forum |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624105951 |
DOIs | |
State | Published - 2020 |
Externally published | Yes |
Event | AIAA Scitech Forum, 2020 - Orlando, United States Duration: Jan 6 2020 → Jan 10 2020 |
Publication series
Name | AIAA Scitech 2020 Forum |
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Volume | 1 PartF |
Conference
Conference | AIAA Scitech Forum, 2020 |
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Country/Territory | United States |
City | Orlando |
Period | 01/6/20 → 01/10/20 |
Funding
We gratefully acknowledge funding from the Natural Sciences and Engineering Research Council (NSERC) of Canada, the Consortium for Aerospace Research and Innovation in Canada (CARIC), the Consortium for Research and Innovation in Aerospace in Québec (CRIAQ), Bombardier Aerospace, Cray Inc. and the McGill University Faculty of Engineering. We gratefully acknowledge funding from the Natural Sciences and Engineering Research Council (NSERC) of Canada, the Consortium for Aerospace Research and Innovation in Canada (CARIC), the Consortium for Research and Innovation in Aerospace in Qu?bec (CRIAQ), Bombardier Aerospace, Cray Inc. and the McGill University Faculty of Engineering.