Paper
30 August 2022 Study on shear stability of composite stiffened panels based on digital image correlation method
Junchao Yang, Xiangming Chen, Zhe Wang
Author Affiliations +
Proceedings Volume 12309, International Conference on Advanced Manufacturing Technology and Manufacturing Systems (ICAMTMS 2022); 123092S (2022) https://doi.org/10.1117/12.2645434
Event: International Conference on Advanced Manufacturing Technology and Manufacturing System (ICAMTMS 2022), 2022, Shijiazhuang, China
Abstract
Based on digital image correlation method (DIC), the shear stability of two configurations of composite stiffened plates was experimentally studied. The test results show that the buckling load and failure load of I-stiffened panels are 158.2 kN and 282.1 kN respectively, and the main failure models are the debonding of the truss skin interface and skin folding; the buckling load and failure load of M-stiffened panels are 181.9 kN and 292.3 kN respectively, and the main failure modes are consistent with that of T-stiffened panels. Then, a progressive damage failure model of stiffened panels was established to simulate the buckling and post-buckling behaviour. The results show that the buckling mode, buckling load, failure load and failure mode are consistent with the experimental results.
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Junchao Yang, Xiangming Chen, and Zhe Wang "Study on shear stability of composite stiffened panels based on digital image correlation method", Proc. SPIE 12309, International Conference on Advanced Manufacturing Technology and Manufacturing Systems (ICAMTMS 2022), 123092S (30 August 2022); https://doi.org/10.1117/12.2645434
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KEYWORDS
Digital image correlation

Composites

Finite element methods

Skin

Failure analysis

Aircraft structures

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