Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Strength Prediction and Damage Analysis of Composite Joints Based On A Delamination Damage Model
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Northwestern Polytechnical University,Northwestern Polytechnical University,Northwestern Polytechnical University

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TB330.1

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    Abstract:

    Based on the three-dimensional progressive damage analysis and cohesive zone model method, a new progressive damage model capable of numerically simulating the behavior of bolted composite joints comprehensively considering composite in-plane and delamination failure is developed. Through the strength analysis of two typical composite single fastener joints, it demonstrate better agreement with the experiments than the traditional 3-D progressive damage model. By this model, a study of the delamination propagation of the composite joints is performed in this paper, and it is found that the direction of delamination propagation is same with the orientation of fracture. The effect of tightening torque on the strength of composite joints and the suppressing delamination propagation of hole is studied.

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Guo Ziang, Wan Xiaopeng, Li Bo. Strength Prediction and Damage Analysis of Composite Joints Based On A Delamination Damage Model[J]. Advances in Aeronautical Science and Engineering,2014,5(4):

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History
  • Received:December 09,2013
  • Revised:February 23,2014
  • Adopted:March 07,2014
  • Online: June 29,2016
  • Published: