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Y. Qi, L. Hu, X. Lin and H. Liu, “Domain Decomposition for Applications Based on CFD-Grid,” Proceedings of the 2004 IEEE International Conference on Services Computing, Shanghai, 15-18 September 2004, pp. 592-595.

has been cited by the following article:

• TITLE: Multi-Domain Parallel Computing for Strength Analysis of Whole Aircraft Model

  AUTHORS: Xiuhua Chen, Hai Wang, Yubo Ding

  KEYWORDS: Parallel Computing, Whole Aircraft Model, Static Strength, Domain Decomposition

  JOURNAL NAME: Journal of Software Engineering and Applications, Vol.4 No.9, September 29, 2011

  ABSTRACT: In the Windows XP 64 bit operating system environment, several common PC were used to build a cluster system, establishing the distributed memory parallel (DMP) computing system. A finite element model of whole aircraft with about 260 million degrees of freedom (DOF) was developed using three-node and four-node thin shell element and two-node beam element. With the large commercial finite element software MSC.MARC and employing two kinds of domain decomposition method (DDM) respectively, realized the parallel solving for the static strength analysis of the whole aircraft model, which offered a high cost-effective solution for solving large-scale and complex finite element models.