Unidirectional composites under cyclic longitudinal tension develop damage through the accumulation and clustering of fibre-breaks, and through fibre-matrix interface debonding growth; these processes lead to a reduction of the material's load-carrying ability with increasing loading cycles, which raises a challenge to predict the fatigue response of composite structures. This paper proposes the first model in the literature to predict the kinetics of fibre-breakage and their effect on the macroscopic response of unidirectional composites under cyclic longitudinal tension. The model couples (i) a statistical hierarchical scaling law to predict fibre failure with (ii) a Paris law to predict interfacial fatigue damage propagating from broken ...
Fatigue of composite materials is of great concern in load-carrying structures. In fact, most failur...
International audienceEarlier work which successfully modelled the kinetics of fibre breakage in uni...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
Failure of fibre-reinforced composites is affected by fatigue, which increases the challenge in desi...
Several modelling approaches are available in the literature to predict longitudinal tensile failure...
Unidirectional composites under longitudinal tension develop damage through the accumulation and clu...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
International audienceA model to predict the effects of the accumulation of fibre breakages in unidi...
Despite the crucial significance of failure prediction in composites, such an objective remains chal...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
COMPTEST 2006 — 10,11,12 abril 2006 OportoFatigue of composite materials is of great concern in load...
The initiation and progression of fiber damage in on-axis UD glass/epoxy materials under fatigue loa...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) c...
A theoretical framework that underlies an accelerated testing method for unidirectional (UD) composi...
Fatigue of composite materials is of great concern in load-carrying structures. In fact, most failur...
International audienceEarlier work which successfully modelled the kinetics of fibre breakage in uni...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
Failure of fibre-reinforced composites is affected by fatigue, which increases the challenge in desi...
Several modelling approaches are available in the literature to predict longitudinal tensile failure...
Unidirectional composites under longitudinal tension develop damage through the accumulation and clu...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
International audienceA model to predict the effects of the accumulation of fibre breakages in unidi...
Despite the crucial significance of failure prediction in composites, such an objective remains chal...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
COMPTEST 2006 — 10,11,12 abril 2006 OportoFatigue of composite materials is of great concern in load...
The initiation and progression of fiber damage in on-axis UD glass/epoxy materials under fatigue loa...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) c...
A theoretical framework that underlies an accelerated testing method for unidirectional (UD) composi...
Fatigue of composite materials is of great concern in load-carrying structures. In fact, most failur...
International audienceEarlier work which successfully modelled the kinetics of fibre breakage in uni...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...