PARALLEL TRANSIENT ALGORITHM WITH MULTISTEP SUBSTRUCTURE COMPUTATION

被引:4
作者
BENNIGHOF, JK
WU, JY
机构
[1] University of Texas at Austin, Department of Aerospace Engineering and Engineering Mechanics, Austin, TX
关键词
D O I
10.2514/3.10689
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A parallel algorithm for computing the transient response of structures is presented. The computation is parallelized on the basis of a division of the structure into substructures, with each processor computing the response of a substructure independently. Independently computed substructure responses are reconciled directly, rather than iteratively, to obtain the solution of the global problem. The only data required for correcting the independently computed response of a substructure is the interface motion computed independently for other substructures. Reconciliation of substructure responses is not required after every time step; instead, it can be postponed until after the responses have been computed independently for multiple time steps. A numerical example is presented that demonstrates the method and its accuracy.
引用
收藏
页码:984 / 991
页数:8
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