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Buckling Analysis and Experimental Validation of Extension-Twist Multicoupled Laminates
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Muyao Miao1, 3, Minghao Zhang1, 3, Da Cui1, 2, 3, **, Daokui Li1, 3
Chinese Journal of Solid Mechanics | 2025, 46(2) : 244 - 256
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Chinese Journal of Solid Mechanics | 2025, 46(2): 244-256
Research Papers
Buckling Analysis and Experimental Validation of Extension-Twist Multicoupled Laminates
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Muyao Miao1, 3, Minghao Zhang1, 3, Da Cui1, 2, 3, **, Daokui Li1, 3
Affiliations
  • 1College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, 410073
  • 2School of Civil Engineering and Mechanics, Lanzhou University, Lanzhou, 730000
  • 3Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions, Changsha, 410073
Published: 2025-04-23 doi: 10.19636/j.cnki.cjsm42-1250/o3.2024.053
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This paper derives the analytical solution for the buckling load of extension-twist multicoupled laminates. The optimization targets both the buckling load and coupling effect, with verification through simulations and experiments. Using the double trigonometric series method, the analytical solution for the buckling load of the extension-twist multicoupled laminate, simply supported on all four sides and subjected to in-plane compressive loads, is obtained. Based on this, a multi-objective optimization design model for the extension-twist multicoupled laminate is established, with the optimization objectives of maximal buckling load and coupling effect. The optimization is achieved using the sequential quadratic programming (SQP) algorithm, and the laminate with enhanced coupling effect and buckling load is designed. Based on the ply angle sequence of the optimal laminate, numerical simulations and robustness analyses confirm the buckling model. Compared to the simulation results, the analytical solution error for the buckling load of the laminate is within 5%, validating the theoretical framework. Experimental measurements using a multi-directional loading test machine reveal that the discrepancy between measured and theoretical buckling loads is within 3%, further verifying the theory's accuracy. This research provides valuable insights for improving the load-bearing capacity of structures such as wings and wind turbine blades.

extension-twist multicoupled laminates  /  buckling analysis  /  multi-objective optimization design  /  experimental validation
Muyao Miao, Minghao Zhang, Da Cui, Daokui Li. Buckling Analysis and Experimental Validation of Extension-Twist Multicoupled Laminates[J]. Chinese Journal of Solid Mechanics, 2025 , 46 (2) : 244 -256 . DOI: 10.19636/j.cnki.cjsm42-1250/o3.2024.053
Year 2025 volume 46 Issue 2
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Article Info
doi: 10.19636/j.cnki.cjsm42-1250/o3.2024.053
  • Receive Date:2024-11-01
  • Online Date:2026-03-20
  • Published:2025-04-23
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  • Received:2024-11-01
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Affiliations
    1College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, 410073
    2School of Civil Engineering and Mechanics, Lanzhou University, Lanzhou, 730000
    3Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions, Changsha, 410073
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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