In this paper, the finite element method is used to analyze the behaviour of repaired cracks in 2024-T3 aluminum with bonded patches made of unidirectional composite plates. The problem is considered in Mode I condition. First the K I stress intensity factor (SIF) is calculated by the finite element method using displacement correlation technique. Different plate and patch thicknesses and crack lengths are considered in the analyses. Then an equation is determined by using genetic algorithms for the calculation of stress intensity factor without any further finite element analysis. The equation gives reasonably accurate results. © Journal Compilation © 2008 Blackwell Publishing Ltd
In aerospace engineering design, structures with holes and cracks have been widely considered, eithe...
The purpose of this thesis was to investigate crack growth behavior in thick stiffened aluminum plat...
The optimum shape of a patch repair for cracked plates is here determined by applying a biology-bas...
In this paper, the finite element method is used to analyze the behaviour of repaired cracks in 2024...
17-23The finite element method (FEM) is used to analyze the behavior of repaired cracks in 2024-T3 ...
The finite element method (FEM) is used to analyze the behavior of repaired cracks in 2024-T3 alumin...
In this study, for composite patch repairs, the impact degrees of patch configuration and patch size...
Bonded composite repair has been recognized as an effcient and economical method to extend the servi...
Bonded composite-patch repair has been used to transfer load from cracked structures to the reinforc...
International audienceIn this study, the three-dimensional finite element method is used to determin...
Adhesively-bonded patches are used for repair of different types of damages such as holes, notches, ...
© 2019, Strojarski Facultet. All rights reserved. The aim of this paper was to establish and demonst...
The problem of the optimal shape of patch repairs for cracked plates is here examined by applying a ...
In this paper, Charpy impact tests were conducted on cracked aluminum plates repaired with FML compo...
This paper aims to analyze the multi-effects of the glass fiber reinforced polymer (GFRP) composite ...
In aerospace engineering design, structures with holes and cracks have been widely considered, eithe...
The purpose of this thesis was to investigate crack growth behavior in thick stiffened aluminum plat...
The optimum shape of a patch repair for cracked plates is here determined by applying a biology-bas...
In this paper, the finite element method is used to analyze the behaviour of repaired cracks in 2024...
17-23The finite element method (FEM) is used to analyze the behavior of repaired cracks in 2024-T3 ...
The finite element method (FEM) is used to analyze the behavior of repaired cracks in 2024-T3 alumin...
In this study, for composite patch repairs, the impact degrees of patch configuration and patch size...
Bonded composite repair has been recognized as an effcient and economical method to extend the servi...
Bonded composite-patch repair has been used to transfer load from cracked structures to the reinforc...
International audienceIn this study, the three-dimensional finite element method is used to determin...
Adhesively-bonded patches are used for repair of different types of damages such as holes, notches, ...
© 2019, Strojarski Facultet. All rights reserved. The aim of this paper was to establish and demonst...
The problem of the optimal shape of patch repairs for cracked plates is here examined by applying a ...
In this paper, Charpy impact tests were conducted on cracked aluminum plates repaired with FML compo...
This paper aims to analyze the multi-effects of the glass fiber reinforced polymer (GFRP) composite ...
In aerospace engineering design, structures with holes and cracks have been widely considered, eithe...
The purpose of this thesis was to investigate crack growth behavior in thick stiffened aluminum plat...
The optimum shape of a patch repair for cracked plates is here determined by applying a biology-bas...