Ultimate strength of composite laminates with free-edge delamination-Reference-Cited by-同舟云学术

Ultimate strength of composite laminates with free-edge delamination

Published:1999-07 Issue:7 Volume:13 Page:569-574
ISSN:1226-4865
Container-title:KSME International Journal
language:en
Short-container-title:KSME International Journal

Author:

Kim In-Kweon,Kang Hyo-Gyoung,Onohara Kaoru

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF03186447.pdf

Reference12 articles.

1. Pipes, R. B. and Pagano, N. J., 1970, “Inter-laminar Stresses in Composite Laminates Under Uniform Axial Extension,”J. Compos. Mater., 4, p. 538.

2. O’Brien, T. K., 1982, “Characterization of Delamination Onset and Growth in a Composite Laminate,”ASTM STP 775, p. 140.

3. Aoki, R. and Kondo, K., 1989, “Free-Edge Delaminationn of Anisotropic Composite Laminates,”J. Japan Soc. Aero. Space Sci., 37(420), p. 29. (in Japanese)

4. Whitcomb, J. D. and Raju, I. S., 1985, “Analysis of Interlaminar Stresses in Thick Composite Laminates With and Without Edge Delamination,”Delamination and Debonding of Materials, ASTM STP 876, p. 69.

5. Kunoo, K, Uda, N., Ono, K. and Onohara, K., 1992, “Generalized Quasi-Three Dimensional Analysis of Composite Laminates with Unsym-metrically Located Free-Edge Delaminations,”Theore. Appl. Mech., 41, p. 137.

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