Abstract | ||
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A commonly held view in the turbomachinery community is that finite element methods are not well-suited for very large-scale thermomechanical simulations. We seek to dispel this notion by presenting performance data for a collection of realistic, large-scale thermomechanical simulations. We describe the necessary technology to compute problems with O(107) to O(109) degrees-of-freedom, and emphasise what is required to achieve near linear computational complexity with good parallel scaling. Performance data is presented for turbomachinery components with up to 3.3 billion degrees-of-freedom. The software libraries used to perform the simulations are freely available under open source licenses. The performance demonstrated in this work opens up the possibility of system-level thermomechanical modelling, and lays the foundation for further research into high-performance formulations for even larger problems and for other physical processes, such as contact, that are important in turbomachinery analysis. |
Year | DOI | Venue |
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2018 | 10.1016/j.finel.2018.11.002 | Finite Elements in Analysis and Design |
Keywords | Field | DocType |
Finite element analysis,Multigrid,Parallel computing,Thermomechanical modelling,Turbomachinery | Turbomachinery,Mathematical optimization,Finite element method,Software,Computational science,Scaling,Mathematics,Computation,Computational complexity theory,Scalability | Journal |
Volume | ISSN | Citations |
155 | 0168-874X | 0 |
PageRank | References | Authors |
0.34 | 7 | 3 |
Name | Order | Citations | PageRank |
---|---|---|---|
Christopher N. Richardson | 1 | 4 | 1.16 |
Nathan Sime | 2 | 0 | 0.34 |
Garth N. Wells | 3 | 202 | 20.08 |