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Mechanics of Materials
Volume 35, Issues 3-6, March-June 2003, Pages 463-480
 
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doi:10.1016/S0167-6636(02)00265-X    How to Cite or Link Using DOI (Opens New Window)
Copyright © 2002 Elsevier Science Ltd. All rights reserved.

A continuum damage model for linear viscoelastic composite materials

Rajesh S. Kumar1 and Ramesh TalrejaCorresponding Author Contact Information, E-mail The Corresponding Author

School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150, USA

Received 15 June 2001. 
Available online 5 December 2002.

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Abstract

This paper presents a constitutive model for linear viscoelastic orthotropic solids containing a fixed level of distributed cracks. The model is formulated in a continuum damage mechanics framework using internal variables taken as second rank tensors. Use is made of the correspondence principle for linear viscoelastic solids to define a pseudo strain energy function in the Laplace domain. This function is then expressed as a polynomial in transformed strain and tensorial damage variables using the integrity bases restricted by the initial orthotropic symmetry of the material. The constitutive relationships derived in the Laplace domain are then converted to the time domain by using the inverse Laplace transform. The model is applied to the specific case of cross-ply laminates with transverse matrix cracks. The material coefficient functions appearing in the model are determined by a numerical (finite element) method for one cross-ply laminate configuration at one damage level. Predictions of the viscoelastic response are then made for the same laminate at other damage levels and for other cross-ply laminate configurations at different damage levels. These predictions agree well with independently determined time variations of properties by an analytic method (Kumar and Talreja, 2001, Linear viscoelastic behavior of matrix cracked cross-ply laminates. Mechanics of Materials 33 (3), 139–154) as well as with the numerically calculated values. Extension of the model to incorporate effects of transient temperature, physical aging and moisture is outlined.

Author Keywords: Damage; Viscoelasticity; Internal variables; Constitutive modeling; Continuum damage mechanics; Composite materials; Correspondence principle; Pseudo strain energy function

Article Outline

1. Introduction
1.1. Internal state variables based approach
1.2. Damage in laminated composite materials
2. Correspondence principle and pseudo energies
3. Constitutive equations for damaged linear viscoelastic materials
3.1. Intralaminar cracking in composite laminates
3.2. Determination of the unknown functions
3.3. Prediction of properties using ISV approach and comparison with micromechanics solutions
4. Incorporating the effects of transient temperature, physical aging and moisture
5. Conclusions
References











Mechanics of Materials
Volume 35, Issues 3-6, March-June 2003, Pages 463-480
 
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