Abstract
A new parallel version of the method LU-SGS (Lower-upper symmetric Gauss-Seidel) based on a multilevel decomposition of the unstructured computational mesh is proposed. The advantages of the proposed approach are demonstrated by computing the supersonic flow around the RAM-C geometry. The method is well scalable when a large number of threads are used on the processor Intel Xeon Phi.
Original language | English |
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Pages (from-to) | 1856-1865 |
Number of pages | 10 |
Journal | Computational Mathematics and Mathematical Physics |
Volume | 57 |
Issue number | 11 |
Early online date | 28 Nov 2017 |
DOIs | |
Publication status | Published - Nov 2017 |
Keywords
- computational fluid dynamics
- hypersonic flows
- Intel Xeon Phi
- multithreaded LU-SGS scheme
- unstructured mesh