Results 131 to 140 of about 20,023 (249)

Enhancing Structural Reliability of Composite Adhesive Joints: An Integrated Experimental‐Numerical‐Machine Learning Framework for Material‐Geometric Co‐Optimization

open access: yesPolymer Composites, Volume 47, Issue 18, Page 17023-17048, 20 September 2026.
An integrated experimental, numerical, and explainable machine learning framework for the material‐geometric co‐optimization and multi‐objective Pareto design of robust composite adhesive joints. ABSTRACT The reliability of composite adhesive joints is compromised by non‐linear dependencies between material properties and manufacturing uncertainties ...
Sajjad Karimi
wiley   +1 more source

Potential of Thermoset Polyolefins for FRP Concrete Reinforcing Bars

open access: yesPolymer Composites, Volume 47, Issue 18, Page 16155-16176, 20 September 2026.
Overview of XLPO and pDCPD resins for FRP reinforcing bars, highlighting resin chemistry, key performance characteristics, fiber sizing interactions, and principal degradation mechanisms in concrete environments. ABSTRACT Although thermoset polyolefins offer resistance to hydrolytic degradation and favorable processing characteristics, their potential ...
Osama Omar   +5 more
wiley   +1 more source

Interlaminar shear strength properties of multistitched preform nano composites

open access: yes, 2016
Warp and weft directional interlaminar shear strength properties of the developed two dimensional multistitched multilayer E-glass/polyester woven nano composites were studied.
Kaya, Gaye Yolacan   +2 more
core   +1 more source

INTERLAMINAR FATIGUE OF THICK-SECTION GLASS FABRIC/VINYL ESTER COMPOSITE

open access: yes, 2016
Fiber composite laminates have been widely used in wind energy and other engineering structures. Three-dimensional deformations and stresses are induced in thick laminates structural joints and ply drops.
Li, Liguo 1988-
core  

Geometric Tunability of Interlaminar Resistance

open access: yesComposites Part B: Engineering
Ping Hu   +2 more
openaire   +1 more source

Mode-I interlaminar fracture of carbon-epoxy cross-ply composites

open access: yes
Mode-I double-cantilever beam (DCB) tests were performed on carbon/epoxy [0 /90]12 specimens. The starter crack was created at mid-thickness, between the 0 and 90 mid-layers. During the tests, however, the crack also propagated along the neighbouring 0/
Marques, A.T.   +3 more
core   +1 more source

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