A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling

Ke Liang, Zhen Yin, Qiuyang Hao. A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling. Computers & Mathematics with Applications, 170:42-55, 2024. [doi]

Authors

Ke Liang

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Zhen Yin

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Qiuyang Hao

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