2021
DOI: 10.3390/polym13193404
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Enhancing Impact Energy Absorption, Flexural and Crash Performance Properties of Automotive Composite Laminates by Adjusting the Stacking Sequences Layup

Abstract: In response to the high demand for light automotive, manufacturers are showing a vital interest in replacing heavy metallic components with composite materials that exhibit unparalleled strength-to-weight ratios and excellent properties. Unidirectional carbon/epoxy prepreg was suitable for automotive applications such as the front part of the vehicle (hood) due to its excellent crash performance. In this study, UD carbon/epoxy prepreg with 70% and 30% volume fraction of reinforcement and resin, respectively, w… Show more

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Cited by 9 publications
(6 citation statements)
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“…The damage modes were characterized by combinations of fiber breakage, matrix cracking, fiber/matrix debonding, surface buckling, fiber pull‐out, and delamination. These failure signs were confirmed by Alshahrani and Ahmed 75 . Glass/epoxy composite pipes filled with 3 wt% of Al 2 O 3 shows low matrix fretting, low matrix micro‐cracking and/or low fiber pullout.…”
Section: Resultsmentioning
confidence: 64%
“…The damage modes were characterized by combinations of fiber breakage, matrix cracking, fiber/matrix debonding, surface buckling, fiber pull‐out, and delamination. These failure signs were confirmed by Alshahrani and Ahmed 75 . Glass/epoxy composite pipes filled with 3 wt% of Al 2 O 3 shows low matrix fretting, low matrix micro‐cracking and/or low fiber pullout.…”
Section: Resultsmentioning
confidence: 64%
“…The impact energy obtained in the present investigation from the 3D printed composites is comparable to the traditionally made composite structures. In the previous studies related to the impact energy absorption of the traditionally made composites, impact energy of 1.5–3 J (Quaresimin et al , 2013), 5–25 J (Alshahrani and Ahmed, 2021) and 13–21 J (Belingardi and Vadori, 2003) for carbon-epoxy composites and 41–47 J (Belingardi and Vadori, 2002) for glass-epoxy composites have been observed. However, in all these investigations, the thickness of the final specimen is limited to around 2–2.5 mm.…”
Section: Resultsmentioning
confidence: 96%
“…), the best configuration was given by [(0°/90°) T /0°n/(0°/90°) T ], where (0°/90°) T denotes a fabric reinforcement. Alshahrani et al [155] stated that the highest energy of unidirectional C/E laminates made by the compression molding process was absorbed by the sequence [(0°/90°/45°/−45°) 2 /0°/90°] S . When using C/E tubes, generally, it emerged that longitudinally oriented fibres have less influence on crashworthiness performance compared to hoop (90°)-oriented ones [124,130], due to the dominant folding failure mechanism.…”
Section: Stacking Sequencementioning
confidence: 99%