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Open Access

Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear

Binwen WANGaXiangming CHENa( )Xiasheng SUNbPuhui CHENcZhe WANGaYa’nan CHAIa
Aeronautics Science and Technology Key Laboratory of Full Scale Aircraft Structure and Fatigue, Aircraft Strength Research Institute of China, Xi’an 710065, China
Chinese Aeronautical Establishment, Beijing 100029, China
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results.

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Chinese Journal of Aeronautics
Pages 272-280

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Cite this article:
WANG B, CHEN X, SUN X, et al. Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear. Chinese Journal of Aeronautics, 2022, 35(3): 272-280. https://doi.org/10.1016/j.cja.2021.01.021

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Received: 09 October 2020
Revised: 20 October 2020
Accepted: 16 December 2020
Published: 20 March 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).