NONLINEAR SNAPPING CONSIDERATIONS FOR LAMINATED CYLINDRICAL PANELS

被引：1

作者：

CHIEN, LS

PALAZOTTO, AN

机构：

[1] Department of Aeronautics and Astronautics, Air Force Institute of Technology, Wright-Patterson Air Force Base

来源：

COMPOSITES ENGINEERING | 1992年 / 2卷 / 08期

关键词：

D O I：

10.1016/0961-9526(92)90021-W

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

A higher-order displacement function is incorporated within nonlinear deformation shell theory in order to investigate laminated composite cylindrical shells under large deformation. The second Piola stress and Green strain tensors are used in the formulation. Furthermore, both static and dynamic features of a cylindrical panel during the snapping process are discussed.

引用

页码：631 / 639

页数：9

共 13 条

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