The snap buckling case in a curved composite beam under a closing bending moment is dealt with. A theoretical approach is developed for the non-linear problem of delamination buckling which is likely to occur in curved composite structures. The approach is based on large deflection characterisation of a curved beam, coupled with fracture mechanics concepts. The general solution is applied to analyse a special case in which delamination occurs very close to inner surface of the beam and snap buckling happens in this delaminated thin layer. The effect of the arc angle of delamination crack on the critical load is also studied
A novel analytical model is developed to solve the problem of free vibration of delaminated composit...
Composites laminates are widely used in both civil and military aircraft structures and gases cylind...
This paper proposes a linear elastic fracture mechanics approach for the prediction of plate end deb...
This thesis is concerned with the analysis of curved laminates and sandwich beams with a focus on de...
Two different studies are carried out to understand the influence of geometric parameters on the buc...
The effects of stacking sequences, fiber orientation angles, boundary conditions and delamination nu...
Asymmetric three-point bending of a layered beam containing an interior interface crack is analyzed ...
Delamination is a major failure mode for composite laminates. Such phenomenon can have multiple caus...
ABSTRACT: In this paper, we provide an insight into the governing mechanism of the uni-axial compres...
Lower and upper bounds of the buckling load of a composite beam with two enveloped delaminations are...
An analytical technique was developed to predict the tensile strength of notched curved composite be...
Carbon fiber reinforced polymer (CFRP) laminate having an embedded delamination may exhibit snap-buc...
In this study, crack growth along curved weak interfaces is investigated experimentally and computat...
Analytic expressions for strain energy release rate and Mixed-Mode stress intensity factors in crack...
Delamination failure in a unidirectional curved composite laminate was investigated. The curved lami...
A novel analytical model is developed to solve the problem of free vibration of delaminated composit...
Composites laminates are widely used in both civil and military aircraft structures and gases cylind...
This paper proposes a linear elastic fracture mechanics approach for the prediction of plate end deb...
This thesis is concerned with the analysis of curved laminates and sandwich beams with a focus on de...
Two different studies are carried out to understand the influence of geometric parameters on the buc...
The effects of stacking sequences, fiber orientation angles, boundary conditions and delamination nu...
Asymmetric three-point bending of a layered beam containing an interior interface crack is analyzed ...
Delamination is a major failure mode for composite laminates. Such phenomenon can have multiple caus...
ABSTRACT: In this paper, we provide an insight into the governing mechanism of the uni-axial compres...
Lower and upper bounds of the buckling load of a composite beam with two enveloped delaminations are...
An analytical technique was developed to predict the tensile strength of notched curved composite be...
Carbon fiber reinforced polymer (CFRP) laminate having an embedded delamination may exhibit snap-buc...
In this study, crack growth along curved weak interfaces is investigated experimentally and computat...
Analytic expressions for strain energy release rate and Mixed-Mode stress intensity factors in crack...
Delamination failure in a unidirectional curved composite laminate was investigated. The curved lami...
A novel analytical model is developed to solve the problem of free vibration of delaminated composit...
Composites laminates are widely used in both civil and military aircraft structures and gases cylind...
This paper proposes a linear elastic fracture mechanics approach for the prediction of plate end deb...