This Part 2 paper presents results of comparative experimental study of progressive damage in 2D and 3D woven glass/epoxy composites under in-plane tensile loading. As Part 1, this Part 2 work is focused on the comparison of in-plane tensile properties of two non-crimp single-ply 3D orthogonal weave E-glass fibre composites on one side and a laminate reinforced with four plies of E-glass plain weave on the other. The damage investigation methodology combines mechanical testing with acoustic emission registration (that provides damage initiation thresholds), progressive cracks observation on transparent samples, full-field surface strain mapping and cracks observation on micrographs, altogether enabling for a thorough characterisation of the...
This research paper examines the damage mechanisms and reductions to the tensile properties of E-gla...
The aim of this study was to understand the low-velocity impact energy absorption mechanism of the d...
ABSTRACT: A testing failure mechanism for 3 were manufactured using mechanical property, the inplane...
This Part 2 paper presents results of comparative experimental study of progressive damage in 2D and...
Composites fabricated by VARTM technology with the use of single-ply non-crimp 3D orthogonal woven p...
The paper studies tension-tension fatigue behavior of a single-ply non-crimp 3D orthogonal weave E-g...
The paper studies tension–tension fatigue behavior of a single-ply non-crimp 3D orthogonal weave Egl...
This paper presents results of a comparative experimental study of the tensile-tensile fatigue behav...
ABSTRACT: The effects of reinforcement geometry, in 2D and 3D woven fabric-reinforced composites, on...
Delamination between layers in composite materials is a major structural failure. The delamination r...
Damage development in transparent woven glass fibre reinforced epoxy laminates manufactured from two...
The use of knitting technology with advanced fibres such as glass, carbon and aramid, to produce nea...
The present study focuses on the mechanical performance and damage evolution of woven fabric E-glass...
peer-reviewedThe use of traditional two-dimensional (2D) fibre preforms can be associated with poor ...
International audienceThe in-plane compressive behavior of two- and three-dimensional woven composit...
This research paper examines the damage mechanisms and reductions to the tensile properties of E-gla...
The aim of this study was to understand the low-velocity impact energy absorption mechanism of the d...
ABSTRACT: A testing failure mechanism for 3 were manufactured using mechanical property, the inplane...
This Part 2 paper presents results of comparative experimental study of progressive damage in 2D and...
Composites fabricated by VARTM technology with the use of single-ply non-crimp 3D orthogonal woven p...
The paper studies tension-tension fatigue behavior of a single-ply non-crimp 3D orthogonal weave E-g...
The paper studies tension–tension fatigue behavior of a single-ply non-crimp 3D orthogonal weave Egl...
This paper presents results of a comparative experimental study of the tensile-tensile fatigue behav...
ABSTRACT: The effects of reinforcement geometry, in 2D and 3D woven fabric-reinforced composites, on...
Delamination between layers in composite materials is a major structural failure. The delamination r...
Damage development in transparent woven glass fibre reinforced epoxy laminates manufactured from two...
The use of knitting technology with advanced fibres such as glass, carbon and aramid, to produce nea...
The present study focuses on the mechanical performance and damage evolution of woven fabric E-glass...
peer-reviewedThe use of traditional two-dimensional (2D) fibre preforms can be associated with poor ...
International audienceThe in-plane compressive behavior of two- and three-dimensional woven composit...
This research paper examines the damage mechanisms and reductions to the tensile properties of E-gla...
The aim of this study was to understand the low-velocity impact energy absorption mechanism of the d...
ABSTRACT: A testing failure mechanism for 3 were manufactured using mechanical property, the inplane...