4.0 Article

Experimental and numerical investigations on the micro-damage behaviour of glass fibre-reinforced plastics

Journal

COMPOSITES PART C: OPEN ACCESS
Volume 10, Issue -, Pages -

Publisher

ELSEVIER
DOI: 10.1016/j.jcomc.2022.100341

Keywords

Glass fibres; Debonding; Micro-mechanics; Non-destructive testing; Ultrasonics

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This study investigates the formation and influence of micro-damage in glass fibre-reinforced plastics (GFRP) through numerical and experimental investigations. It is found that a [0 degrees/90 degrees] layup is the most suitable to generate reproducible micro-damage in the 90 degrees layers. The study also reveals that transverse loading causes a significant loss of shear stiffness and strength.
The formation and influence of micro-damage in glass fibre-reinforced plastics (GFRP) is carried out by numerical and experimental investigations. A quasi-static material characterisation is performed and the stiffness and strength of unidirectional, undamaged material in longitudinal and transverse direction as well as in the 23-plane are determined. Since the desired micro-damage could not be generated in unidirectional laminates due to abrupt failure, a [0 degrees/90 degrees], layup has been identified to be most suitable to generate micro -damage in a reproducible way in the 90 degrees layers, which is done using a tension-tension fatigue test program. During these experiments, micro-damage is detected optically and by means of ultrasonic birefringence, where the latter method shows a reduction in shear modulus due to fibre-matrix debonding prior to final inter -fibre failure. The shear modulus degradation is indirectly measured by the change in the velocity of sound. Since this method is limited to measurements in the 13-and 23-plane, all experiments are accompanied with microstructural simulations with detailed statistical volume elements (SVE), to study the influence of micro -damage under various loading conditions and directions. For loading in fibre direction, no influence on the mechanical properties is observed for the investigated fibre-matrix debonding. However, this is different for transverse loading, where a transverse shear stiffness loss of around 8% results in a decrease of transversal stiffness of around 18%, if the load direction is perpendicular to the damage plane. A similar behaviour is observed for the strength, which is reduced by a factor of 2 for the same configuration.

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