2019
DOI: 10.1016/j.optlastec.2019.03.015
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The influences of laminated structure on the ablation characteristics of carbon fiber composites under CW laser irradiation

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Cited by 12 publications
(4 citation statements)
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“…The dimensions of the tensile test specimen were 120  10  2 mm (length  width  thickness) in accordance with GB/T 3354-1999. Regarding a three-point bending test specimen, the dimensions were 80  10 4 mm T A B L E 1 Thermophysical parameters of carbon fiber and PLA [34,35] Parameter Unit Carbon fiber PLA The shear specimens were printed according to recommendations of ASTM D3163 standard (Standard test method for determining the strength of adhesively bonded rigid plastic lap-shear joints in shear by tension loading). All specimens were printed with concentric paths, as illuminated in Figure 5A.…”
Section: Specimen Configuration and Printing Conditionsmentioning
confidence: 99%
“…The dimensions of the tensile test specimen were 120  10  2 mm (length  width  thickness) in accordance with GB/T 3354-1999. Regarding a three-point bending test specimen, the dimensions were 80  10 4 mm T A B L E 1 Thermophysical parameters of carbon fiber and PLA [34,35] Parameter Unit Carbon fiber PLA The shear specimens were printed according to recommendations of ASTM D3163 standard (Standard test method for determining the strength of adhesively bonded rigid plastic lap-shear joints in shear by tension loading). All specimens were printed with concentric paths, as illuminated in Figure 5A.…”
Section: Specimen Configuration and Printing Conditionsmentioning
confidence: 99%
“…Based on the bridging theory, Liu et al [13] proposed a multiscale progressive damage model of carbon/epoxy composites under laser mechanical coupling, which can effectively predict the failure load of laminates. Nan et al [14] studied the ablation process of composite laminates under CW laser irradiation through tests and simulations. They found that the difference in thermal conductivity of material components and the layup scheme of laminates have a great effect on the ablation morphology.…”
Section: Introductionmentioning
confidence: 99%
“…There have been many studies on CFRP under laser irradiation, involving the influence of layer structure [2,3] , tangential airflow [4,5] and thermal stress [6,7] . And there are also simulation calculations about interlayer crack formation [2,3,8] .…”
Section: Introductionmentioning
confidence: 99%
“…There have been many studies on CFRP under laser irradiation, involving the influence of layer structure [2,3] , tangential airflow [4,5] and thermal stress [6,7] . And there are also simulation calculations about interlayer crack formation [2,3,8] . It has been proved that the peak power density and pulse width of multiple laser are the reasons for the ablation of the matrix and carbon fiber, while increasing the repetition rate and irradiation time can only expand the ablation area of the matrix [9,10] .…”
Section: Introductionmentioning
confidence: 99%