Structural Reliability Analysis for UAV Center Wing Based on Stochastic Finite Element

Da Qian Zhang; Xin Ping Fu; Xiao Dong Tan

doi:10.4028/www.scientific.net/AMM.684.208

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 684Structural Reliability Analysis for UAV Center...

Structural Reliability Analysis for UAV Center Wing Based on Stochastic Finite Element

Abstract:

In general it is difficult to obtain the results directly during process of structural reliability designing because of the complexity of the structure. It can calculate the structure reliability and failure probability effectively according to the combination of finite element method and theory of reliability. This paper introduces a method of structure reliability based on finite element method, summarizes a common method which has an important engineering application value to calculate the reliability such as using Monte-Carlo method to calculate reliability analysis combining with finite element method, recommends a common used software to reliability design and shows the process of using the software to reliability analysis.

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Proceedings of 2014 International Conference on Mechanics and Mechanical Engineering

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Periodical:

Applied Mechanics and Materials (Volume 684)

Pages:

208-212

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.684.208

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Online since:

October 2014

Authors:

Da Qian Zhang*, Xin Ping Fu, Xiao Dong Tan

Keywords:

Central Wing, Monte-Carlo Method, Reliability Analysis, Stochastic Finite Element Method, UAV

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* - Corresponding Author

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