In-situ X-ray computed tomography and online stiffness monitoring were used to study damage initiation and propagation in multi-directional carbon fiber reinforced composite coupon subjected to tension-tension fatigue loading. It was found that a resolution of the CT system of 8 µm was sufficient to capture matrix crack inside the specimen. A clear correlation was found between the increasing number of matrix cracks and the observed stiffness degradation of the composite specimen
The initial stage of fatigue failure has not been thoroughly clarified for carbon fiber reinforced p...
AbstractThe development of fatigue damage in a glass fibre modified layer-to-layer three dimensional...
Whilst quality standards and damage tolerance techniques are unique for each industry, within the ai...
The development and improvement of advanced materials is strictly connected to the understanding of ...
The data published with this article are high resolution X-ray computed tomography (CT) data obtaine...
Fibrous composites are used throughout the aerospace industry with military, commercial, satellite, ...
The development of advanced materials and their improvement is strictly connected to the understandi...
Micromechanisms of fatigue failure in double-notch cross-ply carbon/epoxy coupons have been investig...
In situ fatigue experiments using synchrotron X-ray computed tomography (SRCT) are used to assess th...
In this study, Computed Tomography (CT) is employed to characterize service defects in polymer compo...
Laminated fibre reinforced polymer matrix composites have been used in design and manufacture for mo...
Currently, composite components are widely adopted in aerospace applications but typically over-desi...
A phenomenological study was carried out on laminated carbon fibre-reinforced polymer composites sub...
The data published with this paper is obtained during fatigue testing of a unidirectional non-crimp ...
This paper presents the results of characterization of damage in polymer composite materials that ar...
The initial stage of fatigue failure has not been thoroughly clarified for carbon fiber reinforced p...
AbstractThe development of fatigue damage in a glass fibre modified layer-to-layer three dimensional...
Whilst quality standards and damage tolerance techniques are unique for each industry, within the ai...
The development and improvement of advanced materials is strictly connected to the understanding of ...
The data published with this article are high resolution X-ray computed tomography (CT) data obtaine...
Fibrous composites are used throughout the aerospace industry with military, commercial, satellite, ...
The development of advanced materials and their improvement is strictly connected to the understandi...
Micromechanisms of fatigue failure in double-notch cross-ply carbon/epoxy coupons have been investig...
In situ fatigue experiments using synchrotron X-ray computed tomography (SRCT) are used to assess th...
In this study, Computed Tomography (CT) is employed to characterize service defects in polymer compo...
Laminated fibre reinforced polymer matrix composites have been used in design and manufacture for mo...
Currently, composite components are widely adopted in aerospace applications but typically over-desi...
A phenomenological study was carried out on laminated carbon fibre-reinforced polymer composites sub...
The data published with this paper is obtained during fatigue testing of a unidirectional non-crimp ...
This paper presents the results of characterization of damage in polymer composite materials that ar...
The initial stage of fatigue failure has not been thoroughly clarified for carbon fiber reinforced p...
AbstractThe development of fatigue damage in a glass fibre modified layer-to-layer three dimensional...
Whilst quality standards and damage tolerance techniques are unique for each industry, within the ai...