The Static Strength Reliability Analysis of Composite Aircraft Structures

Long Xiang Lin; Hao Lei Mou; Jian Ren; Tian Chun Zou

doi:10.4028/www.scientific.net/AMM.488-489.1215

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 488-489The Static Strength Reliability Analysis of...

The Static Strength Reliability Analysis of Composite Aircraft Structures

Abstract:

The static strength design of aircraft structure is the most basic design principles. The basic applicable conditions of composite structures static strength reliability analysis using the current methods were mentioned in this paper, and compliance analysis of these basic conditions was carried out. In addition, further studies were also conducted to research the influence of the number of full-scale structural specimens and environmental factors on the composite structures static strength reliability.

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Periodical:

Applied Mechanics and Materials (Volumes 488-489)

Pages:

1215-1218

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.488-489.1215

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Online since:

January 2014

Authors:

Long Xiang Lin*, Hao Lei Mou, Jian Ren, Tian Chun Zou

Keywords:

Aircraft Structure, Composite, Reliability Analysis, Static Strength

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* - Corresponding Author

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