Strength Analysis for Composite Windshield of Commercial Aircraft

Ya Xiong Du; Shu Li; Kai Guo

doi:10.4028/www.scientific.net/AMR.1030-1032.1010

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1030-1032Strength Analysis for Composite Windshield of...

Strength Analysis for Composite Windshield of Commercial Aircraft

Abstract:

With the development of advanced composites technology, composites instead of traditional aluminum alloy, will be widely used to build full-size aircraft windshield structure in the aviation field. The finite element model of commercial aircraft composite windshield is established in the environment of Msc.Patran / Nastran. And based on Tasi-Wu failure criterion, the strength of windshield structure under typical load pressure is predicted and analyzed during failure processes. It shows that composite windshield can work better through rational design according to the analysis result.

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Periodical:

Advanced Materials Research (Volumes 1030-1032)

Pages:

1010-1013

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1010

Citation:

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Online since:

September 2014

Authors:

Ya Xiong Du*, Shu Li, Kai Guo

Keywords:

Composite Windshield Structure, Finite Element Model (FEM), Msc.Patran Nastran, Strength Analysis

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* - Corresponding Author

References

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