Buckling Analysis for Laminated Composite Plates Reinforced by Curvilinear Fibers(Dynamics & Design Conference 2009)
Author:
Affiliation:
1. Division of Human Mechanical Systems and Design, Faculty of Engineering, Hokkaido University
Publisher
Japan Society of Mechanical Engineers
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials
Link
https://www.jstage.jst.go.jp/article/kikaic1979/76/765/76_KJ00006396172/_pdf
Reference16 articles.
1. 1) HYER M. H. The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Composite Structures. (1991) vol.18, p.239-261.
2. 2) GURDAL Z. In-plane response of laminates with spatially varying fiber orientation : variable stiffness concept. AIAA Journal. (1993) vol.31, no.4, p.751-758.
3. 3) LOPES C. S. Progressive failure analysis of tow-placed, variable-stiffness panels. International Journal of Solids and Structures. (2007) vol.44, p.8493-8516.
4. 4) HUNG J. Optimization of fiber orientations near a hole for increased load-carrying capacity of composite laminates. Structural Multidisciplinary Optimization. (2005) vol.30, p.335-341.
5. 5) LOPES C. S. Variable-stiffness Composite Panels : Buckling and First-ply Failure Improvements over Straight-fibre Laminates. Computers & Structures. (2008) vol.86, p.897-907.
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