Parameters Setting Impact Analysis of Composite Cockpit Finite Element Analysis Based on Properties of Composite Materials

Hai Peng Gao; Meng Liu; Jun Wang

doi:10.4028/www.scientific.net/AMR.738.103

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 738Parameters Setting Impact Analysis of Composite...

Parameters Setting Impact Analysis of Composite Cockpit Finite Element Analysis Based on Properties of Composite Materials

Abstract:

At present, mechanics properties of composite at home and abroad only include data of the single-layer board. On the basis of researching literature of composite finite element analysis, approaches of setting composite three-dimensional parameters based on the parameters of single-layer material are summarized. By three-dimensional finite element analysis on composite whole cockpit, the impact of uncertain parameters on cockpit analysis results is studied. Adopting maximum stress criteria, maximum strain criteria and Tsai-Wu criteria to evaluate the initial failure of composite whole cockpit, the impact of material uncertain parameters on initial breaking strength prediction of cockpit is studied. The study can provide reference for three-dimensional finite element analysis of composite whole cockpit.

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Periodical:

Advanced Materials Research (Volume 738)

Pages:

103-106

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.738.103

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Online since:

August 2013

Authors:

Hai Peng Gao, Meng Liu, Jun Wang

Keywords:

Composite Cockpit, Failure Criteria, Finite Element, Impact Analysis, Material Parameters

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