Large Scale Parallel Computing for Fluid Dynamics on Unstructured Grid

被引：1

作者：

Tang, Jing ^{[1
]}

Li, Bin ^{[2
]}

Chen, Jiangtao ^{[2
]}

Gong, Xiaoquan ^{[2
]}

机构：

[1] Northwestern Polytech Univ, Sch Aeronaut, Xian, Shaanxi, Peoples R China

[2] China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang, Peoples R China

来源：

2016 15TH INTERNATIONAL SYMPOSIUM ON PARALLEL AND DISTRIBUTED COMPUTING (ISPDC) | 2016年

关键词：

large scale; parallel computing; fluid dynamics; unstructured grid;

D O I：

10.1109/ISPDC.2016.17

中图分类号：

TP3 [计算技术、计算机技术];

学科分类号：

0812 ;

摘要：

Massive parallel computational fluid dynamics is a vital tool for the modern aviation industry. The parallel aerodynamics numerical simulation software based on unstructured mixed grid and cell-centered finite volume method (FVM) was presented in this paper, which was developed for the complicated configurations of industrial grade. The algorithms for parallel implementation with message passing interface (MPI), including compact numerical discrete schemes, grid partition method for multiprocessors and data transfer scheme, are discussed in detail. The validity of parallel computing is verified using a revolving model of relatively small grid. Then a large transport airplane configuration with hundred millions of grid elements is used for parallel testing, and the efficiency is preserved above 80% up to 18816 processors.

引用

页码：64 / 69

页数：6

共 16 条

[1]

[Anonymous], 2013, 21 AIAA COMP FLUID D

[2]

Berger M. J., 2005, J PARALLEL DISTRIBUT, V65

[3]

Blazek J, 2015, COMPUTATIONAL FLUID

[4]

Horlock J., 2005, J TURBOMACH, P5

[5] Iteration and Parallel Computation on Computational Fluid Dynamics [J].

Huang Xin-cheng ;

Xiao Ai-ling .

2014 7TH INTERNATIONAL CONFERENCE ON INTELLIGENT COMPUTATION TECHNOLOGY AND AUTOMATION (ICICTA), 2014, :318-321

[6] A fast and high quality multilevel scheme for partitioning irregular graphs [J].

Karypis, G ;

Kumar, V .

SIAM JOURNAL ON SCIENTIFIC COMPUTING, 1998, 20 (01) :359-392

[7]

Kim J., 2002, 40 AIAA AER SCI M EX

[8]

Knight D., 1996, AGARD C P PROGR CHAL

[9]

Pan S., 2012, ENG SCI

[10] Early development of implicit methods for Computational Fluid Dynamics at NASA Ames [J].

Pulliam, T. H. .

COMPUTERS & FLUIDS, 2009, 38 (03) :491-495

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