ABSTRACT: The mixed-mode fracture of matrix dominated composite laminates con-taining central holes and cracks was studied using some graphite/epoxy off-axis AS4/3502 balanced symmetric laminates, [±ϕ2]. The uniaxial failure of a 0° laminate, which is the main load carrier of multidirectional laminates, was also investigated. Interesting results were observed for the [± ϕ2]s laminates with a central normal crack. In this paper, the terms "notch sensitivity " and the "notched shape sensitivity " are distinguished, defined and classified with examples. Anisotropic finite width correction factors were applied to inter-polate the experimental data. In general, the predicted not...
Matrix ply cracking is the most common damage to form when a laminate is loaded, and is of considera...
Quantitative understanding of the parameters which control composite fracture is imperative to the i...
Matrix cracks and their effect on ultimate laminate strength in (0/90), ($\pm$45/90), and ($\pm$45/0...
ABSTRACT: Mixed-mode matrix fracture in central notched off-axis unidirectional composite laminates ...
Predicting the residual strength of composite laminates in the presence of flaws such as cracks has ...
Multidirectional laminates are very often used in advanced structures. However, the existing data in...
International audienceThis work studies the behaviour of multidirectional composite laminate under o...
This paper reports a study of the mixed mode I + II fracture of carbon/epoxy unidirectional and mult...
Failure process of continuous fiber reinforced composite laminates in tension usually starts with ap...
Abstract: The object of this work is the study of the behaviour of composite multidirectional lamina...
Fracture and notch-strength tests of graphite-epoxy composites have shown that unidirectional lay-up...
Lamination of composite structures is one of the most common manufacturing techniques used in the co...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
Failure mechanisms in fiber composites are a function of many parameters such as constituent propert...
Quantitative understanding of the parameters which control composite fracture is imperative to the i...
Matrix ply cracking is the most common damage to form when a laminate is loaded, and is of considera...
Quantitative understanding of the parameters which control composite fracture is imperative to the i...
Matrix cracks and their effect on ultimate laminate strength in (0/90), ($\pm$45/90), and ($\pm$45/0...
ABSTRACT: Mixed-mode matrix fracture in central notched off-axis unidirectional composite laminates ...
Predicting the residual strength of composite laminates in the presence of flaws such as cracks has ...
Multidirectional laminates are very often used in advanced structures. However, the existing data in...
International audienceThis work studies the behaviour of multidirectional composite laminate under o...
This paper reports a study of the mixed mode I + II fracture of carbon/epoxy unidirectional and mult...
Failure process of continuous fiber reinforced composite laminates in tension usually starts with ap...
Abstract: The object of this work is the study of the behaviour of composite multidirectional lamina...
Fracture and notch-strength tests of graphite-epoxy composites have shown that unidirectional lay-up...
Lamination of composite structures is one of the most common manufacturing techniques used in the co...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
Failure mechanisms in fiber composites are a function of many parameters such as constituent propert...
Quantitative understanding of the parameters which control composite fracture is imperative to the i...
Matrix ply cracking is the most common damage to form when a laminate is loaded, and is of considera...
Quantitative understanding of the parameters which control composite fracture is imperative to the i...
Matrix cracks and their effect on ultimate laminate strength in (0/90), ($\pm$45/90), and ($\pm$45/0...