Time-Dependent Internal Damage Progress and Residual Strength in Notched Composite Laminates-Reference-Cited by-同舟云学术

Time-Dependent Internal Damage Progress and Residual Strength in Notched Composite Laminates

Published:2012 Issue:6 Volume:6 Page:701-710
ISSN:1880-9871
Container-title:Journal of Solid Mechanics and Materials Engineering
language:en
Short-container-title:JMMP

Author:

KOYANAGI Jun¹,ADACHI Yu²,ARIKAWA Shuichi²,YONEYAMA Satoru²

Affiliation:

1. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

2. Department of Mechanical Engineering, Aoyama Gakuin University

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/jmmp/6/6/6_701/_pdf

Reference8 articles.

1. (2) Koyanagi, J., Yoneyama, S., Eri, K., Shah, P. D., Time dependency of carbon/epoxy interface strength, Composite Structures, Vol. 92 (2010), pp. 150-154.

2. (4) Pierron, F., Green, B., Wisnom, M.R., Full-field assessment of the damage process of laminated composite open-hole tensile specimens. Part I: Methodology, Composites Part A, Vol. 38 (2007), pp. 2307-2320.

3. An experimental investigation into the tensile strength scaling of notched composites

4. On failure mechanisms of composite laminates with an open hole subjected to compressive load

5. An experimental and numerical investigation into the damage mechanisms in notched composites

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