Assessment of crack suppression in glass/epoxy curved laminates by incorporating micro and nanofillers

The design of structures with a large radius of curvature is challenging because fiber‐reinforced composite materials have low resistance to delamination in the direction perpendicular to their thickness. These structures are commonly found in a wide variety of structural components that are used in the wind turbine and aviation industries. The objective of this study is to conduct an experimental investigation into the efficacy of incorporating milled glass fiber, cellulose nanoparticles, and carbon nanoparticles as fillers into an epoxy matrix to improve the resistance to delamination of glass/epoxy curved laminates and thereby inhibit crack growth. In contrast to the baseline samples, curved samples containing 3% cellulose nanoparticles demonstrated enhanced curved beam strength and interlaminar tensile strength by 4.95% and 3.82%, respectively. Additionally, filler‐loaded samples exhibited reduced delamination and fracture propagation damage compared with baseline samples. The adhesion between the epoxy matrix and infill was investigated by means of Fourier transform infrared analysis. In addition, live photographic images and fractured micrographs were correlated with mechanical findings in order to assess delamination suppression and damage processes in both the arm and arc directions. Effect of fillers on delamination ressitance of curved laminates.