Lower bound buckling loads for design of laminate composite cylinders

被引:2
作者
Croll J.G.A. [1 ]
Wang H. [2 ]
机构
[1] Department of Civil and Environmental and Geomatic Engineering, University College London, London
[2] Department of Naval Architecture and Ocean Engineering, China University of Petroleum, Qingdao
来源
Croll, James G. A. (j.croll@ucl.ac.uk) | 1600年 / Bellwether Publishing, Ltd.卷 / 18期
关键词
Analytical; buckling; composites; design; imperfection sensitivity; laminates; lower bounds; shells;
D O I
10.1080/15502287.2016.1273016
中图分类号
学科分类号
摘要
Over a period of more than 45 years, an extensive research program has allowed a series of very simple propositions, relating to the safe design of shells experiencing imperfection sensitive buckling, to be recast in the form of a series of lemmas. These are briefly summarized and their practical use is illustrated in relation to the prediction of safe lower bounds to the imperfection sensitive buckling of axially loaded, fiber reinforced polymeric, laminated cylinders. With a fundamental aspect of the approach, sometimes referred to as the reduced stiffness method, being the delineation of the various shell membrane and bending stiffness (or perhaps more appropriately energy) components contributing to the buckling resistance, the method will be shown to also provide a powerful way of making rational design decisions to optimize the use of fiber reinforcement. © 2017 Taylor & Francis Group, LLC.
引用
收藏
页码:112 / 115
页数:3
相关论文
共 10 条
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