Document Type : Research Paper

Authors

School of Mechanical Engineering, Iran University of Science and Technology, Tehran, Iran.

Abstract

In recent decades, continuum damage mechanics based models, has been of interest to researchers in the area of damage in composites. These models with considering the effects of damage on the mechanical properties of composites and without considering detailed phenomenon of the damage, can analyze wide range of failure modes, loadings and layups. The aim of this paper is to analyze holed composite laminates using continuum damage mechanics. The general damage theory that serves as the foundation for the model of this paper is the model proposed by Ladeveze, which involves damage and inelastic strains to estimate residual stiffness. The Ladeveze model is implemented in a user material defined subroutine of the ABAQUS software, to analyze four different laminate sequences of [02/902]s, [0/90/0/90]s, [452/-452]s, and [0/90/45/-45]s. The analysis includes initiation and growth of damage parameters, subsequently a parametric study for the influence of diameter of hole and the inelastic strain material constant in Ladeveze model. Hence, it was shown that increasing the hole diameter, reduces the laminate strength, while the inelastic strain material constant is proportional to transverse inelastic strains

Keywords

 
 [1]   Raghavan, P. and Ghosh, S., “A Continuum Damage Mechanics Model for Unidirectional Composites Undergoing Interfacial Debonding,” Mech. Mater., Vol. 37, No. 9, pp. 955–979, 2005.
[2]    Mohammadi, B. Hosseini-Toudeshky, H. and Sadr-Lahidjani, M. H., “Damage Evolution of Laminated Composites Using Continuum Damage Mechanics Incorporate with Interface Element,” Key Eng. Mater., Vol. 385, pp. 277–280, 2008.
[3]    Chaboche, J.-L., “Continuous Damage Mechanics—a Tool to Describe Phenomena Before Crack Initiation,” Nucl. Eng. Des., Vol. 64, No. 2, pp. 233–247, 1981.
[4]    Talreja, R., “Internal Variable Damage Mechanics of Composite Materials,” Yielding, Damage, Fail. Anisotropic Solids, pp. 509–533, 1987.
[5]    Voyiadjis, G. Z., Advances in Damage Mechanics: Metals and Metal Matrix Composites: Metals and Metal Matrix Composites. Elsevier, 2012.
[6]    Barbero, E. J., Finite Element Analysis of Composite Materials Using AbaqusTM. Taylor & Francis, 2013.
[7]    Carl H. T., Mechanics of Fibrous Composites. Wiley New York, 1991.
[8]    Ladeveze, P., “A Damage Computational Method for Composite Structures,” Comput. Struct., Vol. 44, No. 1, pp. 79–87, 1992.
[9]    Ladeveze, P., “A Damage Computational Approach for Composites: Basic Aspects and Micromechanical Relations,” Comput. Mech., Vol. 17, No. 1–2, pp. 142–150, 1995.
[10]  Ladeveze. P, and LeDantec, E., “Damage Modelling of the Elementary Ply for Laminated Composites,” Compos. Sci. Technol., Vol. 43, No. 3, pp. 257–267, 1992.
[11]  Ladevèze, P. Allix, O. Deü, J.-F. and Lévêque, D., “A Mesomodel for Localisation and Damage Computation in Laminates,” Comput. Methods Appl. Mech. Eng., Vol. 183, No. 1, pp. 105–122, 2000.
[12]  Mohammadi, B. Hosseini-Toudeshky, H. Sadr-Lahidjani, M. H. andAivazzadeh, S., “Prediction of Inelastic Behavior of Composite Laminates Using Multi-Surface Continuum Damage-Plasticity,” Adv. Mater. Res., Vol. 47, pp. 773–776, 2008.
[13]  Mohammadi, B. Olia, H. and Hosseini-Toudeshky, H., “Intra and Damage Analysis of Laminated Composites Using Coupled Continuum Damage Mechanics with Cohesive Interface Layer,” Compos. Struct., Vol. 120, pp. 519–530, 2015.
[14] Hosseini-Toudeshky H. and Mohammadi, B., “Coupling of Continuum Damage Mechanics with De-Cohesive Element for Delamination Analysis in Laminated Composites,” Adv. Mater. Res., Vol. 123, pp. 527–530, 2010.
[15]Http://help.solidworks.com/2012/English/SolidWorks/cworks/Iterative_Solution_Methods__Newton-Raphson_(NR)_Scheme.htm, “asass.” .
[16] Hashin, Z., “Failure Criteria for Unidirectional Fiber Composites,” J. Appl. Mech., Vol. 47, No. 2, pp. 329–334, 1980.