Transverse cracking and delamination in cross-ply glass-fiber and carbon-fiber reinforced plastic laminates: Static and fatigue loading

Author:

Berthelot Jean-Marie1

Affiliation:

1. Institut d’Acoustique et de Me´canique, Groupe Composites et Structures Me´caniques, Universite´ du Maine, 72085 Le Mans cedex 9, France, jmberthelot@univ-lemans.fr

Abstract

A review of developments and understanding of transverse cracking and delamination in cross-ply laminates is presented. First, experimental investigations reported in the literature for analyzing the development of transverse cracking are considered. Next, characteristics of different models for evaluating the stress distribution in the damaged laminates are developed. It is shown how these models associated with the statistical description of strength or energy released in the 90° plies make it possible to describe the development of transverse cracking in monotonic or fatigue loading. According to the nature of cross-ply laminates, transverse cracking is not, however, sufficient for describing the development of transverse cracks in 90° plies in the case of monotonic loading. In this case, the delamination process induced at transverse crack tips is to be considered for describing the experimental results. There are 108 references in this review article.

Publisher

ASME International

Subject

Mechanical Engineering

Reference108 articles.

1. Birman V and Byrd LW (2000), Review of fracture and fatigue in ceramic matrix composites, Appl. Mech. Rev. 53(6), 147–174.

2. Garrett KW and Bailey JE (1977), Multiple transverse fracture in 90° cross-ply laminates of a glass fiber reinforced polyester, J. Mater. Sci. 12, 157–168.

3. Parvizi A , Garrett KW, and Bailey JE (1978), Constrained cracking in glass fiber-reinforced epoxy cross-ply laminates, J. Mater. Sci. 13, 195–201.

4. Bailey JE and Parvizi A (1981), On fibre debonding effects and the mechanisms of transverse-ply failure in cross-ply laminates of glass fiber/thermoset composites, J. Mater. Sci. 16, 649–659.

5. Highsmith AL and Reifsnider KL (1982), Stiffness reduction mechanisms in composite laminates, Damage in Composite Materials, ASTM STP 775, KL Reifsnider (ed), 103–117.

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