Evaluation of Constitutive Laws for the Computer Simulation of Fatigue Driven Delamination in Composite Materials
Author(s)
Lopez-Armas, Carlos Alberto
Type
Thesis
Abstract
A simple mathematical model (cylinder model) is proposed and used to evaluate
various constitutive laws used in finite element codes to simulate fatigue-driven
delamination in composite materials.
The cylinder model has one degree of freedom and allows the evaluation of several
parameters of the constitutive laws in an ffcient and accurate way without worrying
about the complex interactions that may arise while using a nite element code. This
cylinder model enabled a large number of analysis to be performed in a relatively
short time and made possible parametric studies with tens of thousands of dfferent
sets of parameter values of the constitutive laws.
Different fatigue degradations strategies have been implemented into the cylinder
model and investigated. A systematic comparison of the different strategies has been
performed and it was found that the behaviour of the different strategies is similar
but with some variations in the sensitivity to the spacing of the springs and to the
size of the increment in the number of loading cycles. The results confirm that the
more accurate results are found for smaller values of these two variables.
A new fatigue degradation strategy is also proposed. It is based on the construction
of a 3-D surface that represents the behaviour of the interface under fatigue
loading. This surface has been incorporated into the cylinder model and its performance
has been evaluated.
various constitutive laws used in finite element codes to simulate fatigue-driven
delamination in composite materials.
The cylinder model has one degree of freedom and allows the evaluation of several
parameters of the constitutive laws in an ffcient and accurate way without worrying
about the complex interactions that may arise while using a nite element code. This
cylinder model enabled a large number of analysis to be performed in a relatively
short time and made possible parametric studies with tens of thousands of dfferent
sets of parameter values of the constitutive laws.
Different fatigue degradations strategies have been implemented into the cylinder
model and investigated. A systematic comparison of the different strategies has been
performed and it was found that the behaviour of the different strategies is similar
but with some variations in the sensitivity to the spacing of the springs and to the
size of the increment in the number of loading cycles. The results confirm that the
more accurate results are found for smaller values of these two variables.
A new fatigue degradation strategy is also proposed. It is based on the construction
of a 3-D surface that represents the behaviour of the interface under fatigue
loading. This surface has been incorporated into the cylinder model and its performance
has been evaluated.
Date Issued
2008-01
Date Awarded
2008-06
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
Advisor
Galvanetto, Ugo
Robinson, Paul
Creator
Lopez-Armas, Carlos Alberto
Publisher Department
Aeronautics
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
Doctor of Philosophy (PhD)