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首页> 外文期刊>Transactions of the Japan society for aeronautical and space sciences >Buckling Modes and Developable Postbuckling Modes of Axially Compressed Short Circular Cylindrical Shells
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Buckling Modes and Developable Postbuckling Modes of Axially Compressed Short Circular Cylindrical Shells

机译：轴向压缩短圆柱圆柱壳的屈曲模式和可展开的后屈曲模式

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摘要

The developability of thin circular cylindrical shells of infinite length leads to the postbuckling modes described by Yoshimura for shells under axial compression. Yamaki et al. calculated and measured experimentally the postbuckling modes of a cylindrical shell of finite length under axial compression. However, they did not calculate the buckling mode of the cylinder. To clarify the entire process of mode changes during buckling and postbuckling, an axial buckling mode is calculated and drawn for the cylinder whose corresponding postbuckling modes have been investigated by Yamaki et al. The axial postbuckling modes of finite length cylinders are shown to be deployable on flat surfaces due to the developability of cylindrical shells.
机译：无限长的薄圆柱壳的可开发性导致Yoshimura描述了轴向压缩壳的后屈曲模式。山木等。计算并实验测量了有限长度的圆柱壳在轴向压缩下的后屈曲模式。但是，他们没有计算圆柱体的屈曲模式。为了弄清屈曲和后屈曲过程中模式变化的整个过程，对Yamaki等人研究了其相应的后屈曲模式的圆柱，计算并绘制了轴向屈曲模式。由于圆柱壳的可发展性，有限长度圆柱的轴向后屈曲模式显示为可在平坦表面上展开。

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