Title of article :
A Continuum Damage Mechanics Approach for Reliability Analysis of Composite Laminates Containing a Central Circular Hole
Author/Authors :
Gholami, Peyman Aerospace Research Institute (Ministry of Science, Research and Technology), Tehran, Iran , Kouchakzadeh, Mohammad Ali Department of Aerospace Engineering - Sharif University of Technology, Tehran, Iran , Farsi, Mohammad Ali Aerospace Research Institute (Ministry of Science, Research and Technology), Tehran, Iran
Abstract :
This paper discusses the topic of probabilistic analysis of composite laminates rectangular plates containing a central circular hole
under static tensile load. First, According to the continuum damage mechanics (CDM) approach, structural analysis models, the
definition of damage and the treatment of random variables will be explored. Then, the matrix cracking and fiber/matrix debonding
damage is modeled and the material constitutive relationships are implemented in the ABAQUS software by the subroutine. The
probabilistic methods, first order reliability method (FORM) and second order reliability method (SORM) have been used to analyze
the composite plates’ system failure probability. The failure functions and random variables have been obtained according to the CDM
approach. Issues arising out of the use of composite material structures, in applications, due to non-homogeneity and anisotropic
characteristics, and manufacturing defects will be highlighted, and uncertainties related to the material properties, loads, and boundary
conditions will be discussed through examples. It is shown that the scatter in parameter values has a significant effect on damage
development in the model.
Keywords :
Matrix Cracking , Fiber/Matrix Debonding , Continuum Damage Mechanics
Journal title :
International Journal of Reliability, Risk and Safety: Theory and Application