Finite Element Based Sub-Laminate Damage Model for Intraply Cracking

Author:

Yang Qinghui,Engblom John J.1

Affiliation:

1. Mechanical & Aerospace Engineering Department, Florida Institute of Technology, Melbourne, FL 3290)

Abstract

An analytical sublaminate model of intralaminar cracking, i.e., representative of a particular ply or sub-set of adjacent plies (layers) of equal orientation, is developed by an internal state variable (ISV) approach. Furthermore, a finite element based plylevel damage formulation is established to represent the variation of material properties with intralaminar cracks. Simple linear and parabolic "layer" material models are shown to be useful in providing for a smooth transition in stiffness characteristics as crack densities increase. The utility of the formulation is established in the comparison of predicted laminate stiffness variation and constitutive relations with experimental results. In addition, some results are presented based on implementation of the ply-level damage model in a finite element formualtion.

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference26 articles.

1. Stiffness changes in unidirectional composites caused by crack systems

2. Analysis of Progressive Matrix Cracking in Composite Laminates I. Thermoelastic Properties of a Ply with Cracks

3. 4. Highsmith, A. L., W. W. Stinchcomb and K. L. Reifsnider. 1984. "Effect of Fatigue-Induced Defects on the Residual Response of Composite Laminates," AS7MSTP 836, pp. 194-216.

4. Analysis of cracked laminates: a variational approach

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