Variable-stiffness composite panels: Defect tolerance under in-plane tensile loading-Reference-Cited by-同舟云学术

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Variable-stiffness composite panels: Defect tolerance under in-plane tensile loading

Published:2014-08 Issue: Volume:63 Page:21-31
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Falcó O.,Mayugo J.A.,Lopes C.S.,Gascons N.,Costa J.

Funder

Ministerio de Economía y Competitividad of Spain

Generalitat de Catalunya

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference35 articles.

1. The engineering aspects of automated prepreg layup: history, present and future;Lukaszewicz;Compos Part B: Eng,2012

2. Lopes CS. Damage and failure of non-conventional composite laminates. PhD thesis. Delft University of Technology; 2009.

3. Variable stiffness panels: effects of stiffness variation on the in-plane and buckling responses;Gürdal;Compos Part A: Appl Sci Manuf,2008

4. Gürdal Z, Tatting BF, Wu KC. Tow-placement technology and fabrication issues for laminated composite structures. In: Proceedings of the Aiaa/Asme/Asce/Ahs/Asc structures, 46th structural dynamics & materials conference; 2005.

5. Optimization of course locations in fiber-placed panels for general fiber angle distributions;Blom;Compos Sci Technol,2010

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