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全机模型静强度分析的多区域并行计算

Multi-domain Parallel Computing for Static Strength Analysis of Whole Aircraft Model

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【作者】 丁玉波陈秀华汪海

【Author】 DING Yu-bo,CHEN Xiu-hua,WANG Hai(School of Aeronautics and Astronautics,Shanghai Jiaotong University,Shanghai 200240,China)

【机构】 上海交通大学航空航天学院

【摘要】 在Windows XP 64位操作系统环境下,利用若干普通PC机搭建了机群系统,实现了分布内存式并行(DMP)计算。采用3节点和4节点薄壳单元和2节点梁单元建立了约260万自由度(DOF)的全机有限元模型。采用封装的METIS区域分解方法(DDM),并利用大型通用有限元软件MSC.Marc,实现了全机静强度模型的并行求解,为大型复杂有限元模型的求解提供了一种高性价比的解决方案。

【Abstract】 In the Windows XP 64 bit operating system environment,several common PC is used to build a cluster system,realizing the distributed memory parallel(DMP) computing.A finite element model of whole aircraft with about 260 million degrees of freedom(DOF) is developed using three-node and four-node thin shell element and two-node beam element.Employing the packaged METIS domain decomposition method(DDM) and making use of the large universal finite element software MSC.Marc,this paper realizes the parallel solving of the static strength model of the whole aircraft,which offers a high cost-effective solution for solving large complex finite element models.

  • 【文献出处】 航空计算技术 ,Aeronautical Computing Technique , 编辑部邮箱 ,2010年05期
  • 【分类号】TP338.6
  • 【被引频次】2
  • 【下载频次】60
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