Quantitative evaluation of fatigue damage growth in CFRP laminates that changes due to applied stress level-Reference-Cited by-同舟云学术

Quantitative evaluation of fatigue damage growth in CFRP laminates that changes due to applied stress level

Published:2011-06 Issue:6 Volume:33 Page:781-787
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Hosoi Atsushi,Takamura Keigo,Sato Narumichi,Kawada Hiroyuki

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference18 articles.

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2. Masters JE, Reifsnider KL. An investigation of cumulative damage development in quasi-isotropic graphite/epoxy laminates. ASTM STP 775; 1982. p. 40–61.

3. Liu S, Nairn JA. Fracture mechanics analysis of composite microcracking: experimental results in fatigue. In: Proceedings of 5th technical conference on composite materials; 1990. p. 287–95.

4. On matrix crack growth in quasi-isotropic laminates − I. Experimental investigation;Tong;Compos Sci Technol,1997

5. On matrix crack growth in quasi-isotropic laminates − II. Finite element analysis;Tong;Compos Sci Technol,1997

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