Effects of set curvature and fiber bundle size on the printed radius of curvature by a continuous carbon fiber composite 3D printer

R Matsuzaki, T Nakamura, K Sugiyama, M Ueda… - Additive …, 2018 - Elsevier
The present study investigated the effects of set radius of curvature and fiber bundle size on
the precision of the radius of curvature during continuous carbon fiber three-dimensional …

Isogeometric analysis of multilayer composite shell structures: Plasticity, damage, delamination and impact modeling

MD Alaydin, M Behzadinasab, Y Bazilevs - International Journal of Solids …, 2022 - Elsevier
A comprehensive Isogeometric Analysis framework for damage modeling of laminated
composite structures is presented. The formulation is based on a multilayer approach that …

Experimental and numerical study on progressive damage and failure in composite laminates during open-hole compression tests

R Higuchi, S Warabi, A Yoshimura… - Composites Part A …, 2021 - Elsevier
Progressive damages in the open-hole compression (OHC) tests of composite laminates
were experimentally and numerically studied. In the experiment, the failure mechanisms …

[HTML][HTML] Automated detection of yarn orientation in 3D-draped carbon fiber fabrics and preforms from eddy current data

G Bardl, A Nocke, C Cherif, M Pooch, M Schulze… - Composites Part B …, 2016 - Elsevier
Ensuring the correct fiber orientation in draped textiles and 3D preforms is one of the current
challenges in the production of carbon-fiber reinforced plastics (CFRP), especially in resin …

[HTML][HTML] Estimation of axial compressive strength of unidirectional carbon fiber-reinforced plastic considering the variability of fiber misalignment

M Ueda, Y Suzuki, ST Pinho - Composites Part A: Applied Science and …, 2023 - Elsevier
The analytical method to calculate the axial compressive stress–strain relation of a
unidirectional carbon fiber-reinforced plastic (UD CFRP) was presented considering the …

Compressive failure strain of unidirectional carbon fibre composites from bending tests

X Wu, MR Wisnom - Composite Structures, 2023 - Elsevier
One of the major difficulties in establishing material properties for composites is to obtain
reliable compressive strengths either from the current direct compressive testing methods …

Effects of fiber properties on aerodynamic performance and structural sizing of composite aircraft wings

S Date, Y Abe, T Okabe - Aerospace Science and Technology, 2022 - Elsevier
An advanced carbon fiber is expected to reduce the structural weight of a composite aircraft.
Historically, various studies on composite aircraft designs have focused on the challenge to …

A new damage model for composite laminates

ML Ribeiro, V Tita, D Vandepitte - Composite Structures, 2012 - Elsevier
Aircraft composite structures must have high stiffness and strength with low weight, which
can guarantee the increase of the pay-load for airplanes without losing airworthiness …

Fatigue life evaluation for carbon/epoxy laminate composites under constant and variable block loading

PNB Reis, JAM Ferreira, JDM Costa… - … Science and Technology, 2009 - Elsevier
This paper presents the results of current research on the fatigue life prediction of
carbon/epoxy laminate composites involving twelve balanced woven bidirectional layers of …

[HTML][HTML] Characterisation of carbon fibre-reinforced polymer composites through radon-transform analysis of complex eddy-current data

RR Hughes, BW Drinkwater, RA Smith - Composites Part B: Engineering, 2018 - Elsevier
Maintaining the correct fibre orientations and stacking sequence in carbon-fibre reinforced
polymers (CFRP) during manufacture is essential for achieving the required mechanical …