Study on global stability of aluminum alloy honeycomb cylinder under axial compression

WEI Jiarui; WU Qiong; WU Wei; LI Qunzhi; SHI Hongwei; ZHANG Yu

doi:10.13700/j.bh.1001-5965.2023.0135

Volume 51 Issue 3

Mar. 2025

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Journal of Beijing University of Aeronautics and Astronautics > 2025 > 51(3): 962-972.

Song Wenbo, Li Huanxi, Lü Mingyun, et al. Effects of thickness and environmental factors on conductivity of composite coatings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(12): 1351-1354. (in Chinese)

Citation:

WEI J R，WU Q，WU W，et al. Study on global stability of aluminum alloy honeycomb cylinder under axial compression[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：962-972 （in Chinese） doi: 10.13700/j.bh.1001-5965.2023.0135

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Study on global stability of aluminum alloy honeycomb cylinder under axial compression

doi: 10.13700/j.bh.1001-5965.2023.0135

WEI Jiarui^{1, 2, 3},
WU Qiong^{1, 2
,
,},
WU Wei⁴,
LI Qunzhi⁵,
SHI Hongwei⁵,
ZHANG Yu^{1, 2}

1.
State Key Laboratory of Virtual Reality Technology and Systems，Beihang University，Beijing 100191，China
2.
Jingdezhen Branch of Jiangxi Research Institute of Beihang University，Jingdezhen 333000，China
3.
The 9th Overall Design Department of China Aerospace Science and Industry Corporation，Wuhan 430040，China
4.
Beijing Aerospace Technology Institute，Beijing 100074，China
5.
Beijing Institute of Spacecraft System Engineering，Beijing 100094，China

Funds: National Natural Science Foundation of China (51875024); Civil Space Technology Pre-Research Program (D020304)

More Information

Corresponding author: E-mail：wuqiong@buaa.edu.cn
Received Date: 23 Mar 2023
Accepted Date: 07 Jul 2023

Available Online: 05 Aug 2023

Publish Date: 03 Aug 2023

Abstract

Abstract

Metal honeycomb cylinder structures frequently encounter a decrease in load-carrying capacity due to axial compression buckling. Extensive research has been conducted on their elastic buckling behavior. However, there are few theoretical studies on their plastic buckling behavior. To address this issue, a theoretical formula was derived for the elastic and plastic buckling critical load of the aluminum alloy honeycomb cylinder under axial compression, drawing upon the equivalent model of the honeycomb cylinder and the Hamilton principle. The simulation analysis and experimentations on the above problem were carried out. Finally, the influence of the honeycomb cylinder dimensional parameters on the critical load was discussed using the theoretical formula. The results show that both the theoretical formula and the simulation model can accurately predict the critical load of the aluminum alloy honeycomb cylinder. In comparison, the theoretical formula is calculated faster. When the cylinder mass changes within the range of ±10%, the influence degree of panel thickness, cylinder radius, core thickness and cylinder height on the critical load decreases successively. The honeycomb cylinder’s critical load exhibits a minor association with the cylinder height, but it exhibits an approximately linear positive correlation with the cylinder radius, core thickness, and panel thickness.
- honeycomb cylinder,
- global stability,
- critical load,
- elasto-plastic,
- Hamilton principle,
- finite element

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References(28)

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