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

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Publication:6590228

DOI10.1016/J.CAMWA.2024.06.014MaRDI QIDQ6590228

Zhen Yin, Ke Liang, Qiuyang Hao

Publication date: 21 August 2024

Published in: Computers & Mathematics with Applications (Search for Journal in Brave)






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