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Full Length Article | Open Access

Experimental and numerical studies on buckling and post-buckling behavior of T-stiffened variable stiffness panels

Yan HUANGaYahui ZHANGb( )Bin KONGcJiefei GUdZhe WANGe,fPuhui CHENa( )
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
AVIC Aviation Power Control System Research Institute, Wuxi 214063, China
Chengdu Aircraft Design and Research Institute, Aviation Industry Corporation of China, Chengdu 610091, China
School of Mechanical Engineering, Jiangnan University, Wuxi 214122, China
School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
China National Key Laboratory of Strength and Structural Integrity, Aircraft Strength Research Institute of China, Xi’an 710065, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Currently, experimental research on variable stiffness design mainly focuses on laminates. To ensure adaptability in practical application, it is imperative to conduct a systematic study on stiffened variable stiffness structures, including design, manufacture, experiment, and simulation. Based on the minimum curvature radius and process schemes, two types of T-stiffened panels were designed and manufactured. Uniaxial compression tests have been carried out and the results indicate that the buckling load of variable stiffness specimens is increased by 26.0%, while the failure load is decreased by 19.6%. The influence mechanism of variable stiffness design on the buckling and failure behavior of T-stiffened panels was explicated by numerical analysis. The primary reason for the reduced strength is the significantly increased load bearing ratio of stiffeners. As experimental investigations of stiffened variable stiffness structures are very rare, this study can be considered a reference for future work.

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Chinese Journal of Aeronautics
Pages 459-470

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Cite this article:
HUANG Y, ZHANG Y, KONG B, et al. Experimental and numerical studies on buckling and post-buckling behavior of T-stiffened variable stiffness panels. Chinese Journal of Aeronautics, 2024, 37(10): 459-470. https://doi.org/10.1016/j.cja.2024.08.015

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Received: 01 November 2023
Revised: 12 December 2023
Accepted: 26 January 2024
Published: 13 August 2024
© 2024 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/).