One of the major difficulties in interlaminar fracture tests of multidirectional laminates is the high tendency for intralaminar cracking and the resulting wavy crack propagation. Experimental work showed that this occurred in double cantilever beam (DCB) tests of cross-ply laminates having a starter crack on a 0degrees/90degrees interface. Moreover, under steady-state propagation conditions, the apparent values of the critical strain energy release rate G(Ic) were two times higher than those of 0degrees/0degrees specimens. In this paper, a finite-element-based progressive damage model was used to simulate crack propagation in cross-ply specimens. The results showed that transverse cracking alone cannot be responsible for the above diff...
The apparent crack resistance curves associated with longitudinal tensile failure of carbon fibre re...
A numerical study was performed on the mode II interlaminar critical strain energy release rate (GII...
The main objective of this thesis was to increase the understanding of interlaminar toughening mecha...
Mode-I double-cantilever beam (DCB) tests were performed on carbon/epoxy [0 /90]12 specimens. The st...
The intralaminar mode I fracture toughness values for a M55J/M18 carbon/epoxy cross-ply laminate [0&...
This paper reports an experimental study on the mode I interlaminar fracture of carbon/epoxy multidi...
An experimental study was conducted on the mode I interlaminar fracture of carbon/epoxy multidirecti...
Cross-ply composite laminates can develop very high density of transverse cracks in the 90-layer und...
The macroscopic failure of composite laminates subjected to tensile increasing load is preceded by i...
ABSTRACT: The mechanics of transverse ply cracking in crossply composite laminates is examined in de...
Failure process of continuous fiber reinforced composite laminates in tension usually starts with ap...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
ABSTRACT: The previously developed closed form expressions for thermo-elastic properties of laminate...
This paper presents numerical analyses of crack propagation in double cantilever beam (DCB) tests of...
Transverse crack propagating towards a cross-ply interface is investigated in this study. The non-un...
The apparent crack resistance curves associated with longitudinal tensile failure of carbon fibre re...
A numerical study was performed on the mode II interlaminar critical strain energy release rate (GII...
The main objective of this thesis was to increase the understanding of interlaminar toughening mecha...
Mode-I double-cantilever beam (DCB) tests were performed on carbon/epoxy [0 /90]12 specimens. The st...
The intralaminar mode I fracture toughness values for a M55J/M18 carbon/epoxy cross-ply laminate [0&...
This paper reports an experimental study on the mode I interlaminar fracture of carbon/epoxy multidi...
An experimental study was conducted on the mode I interlaminar fracture of carbon/epoxy multidirecti...
Cross-ply composite laminates can develop very high density of transverse cracks in the 90-layer und...
The macroscopic failure of composite laminates subjected to tensile increasing load is preceded by i...
ABSTRACT: The mechanics of transverse ply cracking in crossply composite laminates is examined in de...
Failure process of continuous fiber reinforced composite laminates in tension usually starts with ap...
Advanced polymer composites are commonly based on thin prepreg plies stacked at different angles to ...
ABSTRACT: The previously developed closed form expressions for thermo-elastic properties of laminate...
This paper presents numerical analyses of crack propagation in double cantilever beam (DCB) tests of...
Transverse crack propagating towards a cross-ply interface is investigated in this study. The non-un...
The apparent crack resistance curves associated with longitudinal tensile failure of carbon fibre re...
A numerical study was performed on the mode II interlaminar critical strain energy release rate (GII...
The main objective of this thesis was to increase the understanding of interlaminar toughening mecha...