An Amendment Method for Stress and Strain of Double-Curved Laminated Composite

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Abstract:

In this paper, an amendment method for stress and strain of double-curved laminated composite is proposed and studied. According to finite element analysis results of the same model with two different mesh size (coarse mesh size 120mm× 300mm and refined mesh size 30mm× 30mm ), stress and strain have been amended with modified formula in user material subroutine (UMAT) subprogram so that the corrected results of model with coarse mesh is similar to the results of model with refined mesh. Using this method, with coarse mesh, a satisfied accuracy results still can be obtained without refining mesh. It’s efficient for design and analysis of complex structures.

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Periodical:

Materials Science Forum (Volumes 561-565)

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757-760

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Online since:

October 2007

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© 2007 Trans Tech Publications Ltd. All Rights Reserved

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[1] Ahmet Sinan Oktem, Reaz A. Chaudhuri, Composite Structures, Vol. 80(2007), p.475.

Google Scholar

[2] Guang-Hui Qing, Yang-Hong Liu, Jia-Jun Qiu etc., Finite Elements in Analysis and Design, Vol. 42(2006), p.837.

Google Scholar

[3] Meizhen Tao, General Design of Aircraft Structures, (Xi'an: Northwestern Polytechnical University Press, 2001).

Google Scholar

[4] Cheng Honghuo, FEM Samples Based Marc Software, (Beijing: Mechanical Industrial Press, 2003).

Google Scholar