Research progress in post-buckling design and analysis techniques for composite stiffened panel

被引：0
|
作者：
Chen, Xiangming [1 ]
Li, Xinxiang [1 ]
Chai, Yanan [1 ]
Chen, Puhui [2 ]
Sun, Xiasheng [3 ]
机构：
[1] National Key Laboratory of Strength and Structural Integrity, Aircraft Strength Research Institute of China, Xi’an,710065, China
[2] College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
[3] School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, China
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2024年 / 41卷 / 09期
关键词：
Compendex;
D O I：
10.13801/j.cnki.fhclxb.20240611.003
中图分类号：
学科分类号：
摘要：
Buckling loads
引用
收藏
页码：4647 / 4674
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