Post-buckling analysis method of stiffened composite panels and test verification

Post-buckling analysis method of stiffened composite panels and test verification

Post-buckling analysis methods of fiber-reinforced T section stiffened composite panels were investigated. In this paper, the Finite Element Model was presented. In the model, the progressive damage analysis (PDA) and the cohesive zone model (CZM) were used to simulate the damage progression in skin...

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Bibliographic Details
Main Authors: LIN Guowei, LI Xinxiang
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2021-08-01
Series:Journal of Aeronautical Materials
Subjects:
composite
post-buckling
progressive damage analysis
cohesive zone model
finite element model
engineering calculation method
Online Access:http://jam.biam.ac.cn/article/doi/10.11868/j.issn.1005-5053.2021.000013

Internet

http://jam.biam.ac.cn/article/doi/10.11868/j.issn.1005-5053.2021.000013

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