4.7 Article

Multi-objective design optimization of variable stiffness composite cylinders

期刊

COMPOSITES PART B-ENGINEERING
卷 69, 期 -, 页码 249-255

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compositesb.2014.10.011

关键词

Buckling; Computational modelling; Finite element analysis (FEA); Variable stiffness

资金

  1. Natural Sciences and Engineering Research Council of Canada (NSERC) industrial chair on Automated Composites
  2. Bell Helicopter Textron Canada Ltd.
  3. Bombardier Aerospace
  4. Delastek Ltd.
  5. Concordia University

向作者/读者索取更多资源

The bending-induced buckling improvement in a variable stiffness (VS) composite cylinder (made by fiber steering) is studied. For such a cylinder, the effect of the variation of the direction of the load on its buckling performance of the cylinder is also examined. Compromise programming, as a multiobjective optimization method, is used to design for buckling of the VS cylinder subjected to bending load in either of the two opposite directions. Different combinations of weight factors for the structural performance in the two opposite directions were also applied to obtain the Pareto frontier as the main decision making tool for the designers in a multi-objective design problem. (C) 2014 Elsevier Ltd. All rights reserved.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据