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- W4284890231 abstract "The present study reports the low-velocity impact (LVI) performance of carbon woven reinforced polymer (CWRP) composites with varying temperatures. The fabrication of carbon woven lamina and carbon woven reinforced two-layered laminate (named CWRP-1 and CWRP-2) was done using a vacuum-assisted resin transfer molding (VARTM) process. CWRP-1 samples were tested at varying impact velocities of 1, 2, 3, and 4 m/s at − 25, 25, and 50 °C for each incident velocity. CWRP-2 samples were tested at room temperature at varying incident velocities to determine the effect of multiple woven layers. The impact resistance of the first-crack load, peak impact load, and absorbed energies were recorded and evaluated under different loading conditions. In addition, the Weibull probability method is adapted to forecast failure behavior as a function of load. Visual inspection, optical microscopy, and scanning electron microscope (SEM) images were used to assess the damage pattern and failure morphologies in forecasting the failure phases during LVI. The low-velocity impact behavior of CWRP-1 at − 25 °C with various velocities was shown to be random due to the polymer matrix freezing condition. The softening of the resin matrix at 50 °C is responsible for the difference in damage tolerance. The relevance of multiple layered composites for better impact resistance characteristics was demonstrated during testing of CWRP-2 at room temperature. Overall, the results of this experiment showed that CWRP lamina and laminates are highly sensitive to the impact velocities and external temperatures. • Low velocity impact characteristics of single layer lamina and two layered laminates are investigated in this study. • Experimental results suggested that thickness of the composite, incident velocity and external temperature significantly affect the LVI performance. • Temperature variations had a significant impact on the characteristics of the polymer matrix, which is an essential element of composite. • The mechanisms of failure patterns are observed through the SEM images which is capable to represent different failure modes like fiber debonding and fracture." @default.
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- W4284890231 date "2022-10-01" @default.
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- W4284890231 title "Low-velocity impact behavior of carbon woven laminates after exposure to varying temperatures" @default.
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- W4284890231 doi "https://doi.org/10.1016/j.tws.2022.109636" @default.
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