4.7 Article

Stiffness tailoring of elliptical composite cylinders for axial buckling performance

期刊

COMPOSITE STRUCTURES
卷 150, 期 -, 页码 115-123

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2016.05.007

关键词

Stiffness tailoring; Variable stiffness; Elliptical composite cylinder; Buckling; Design optimization

资金

  1. Natural Sciences and Engineering Research Council of Canada (NSERC)
  2. Bell Helicopter Textron Canada Ltd.
  3. Bombardier Aerospace, Delastek Ltd.
  4. Concordia University

向作者/读者索取更多资源

Automated fiber placement (AFP) machines have made it possible to tailor the material stiffness properties in a laminated composite structure by fiber steering. The so-called variable stiffness (VS) laminate can be designed to improve the structural performance of a composite component. Herein, using a meta-modeling based design optimization (MBDO) method, elliptical composite cylinders with VS laminate are designed and optimized for maximum axial buckling capacity. The effect of cross-sectional aspect ratio of the elliptical cylinders on the potential improvement of the buckling capacity is also investigated. As the baseline for comparison, for each cross-sectional aspect ratio, the buckling capacity of elliptical cylinders with quasi-isotropic (QI) and optimum constant stiffness (CS) laminates are also calculated. It is found that the buckling capacity of an elliptical composite cylinder can be improved by fiber steering up to 118% compared with its best CS counterpart. (C) 2016 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