2021
DOI: 10.1016/j.compositesa.2021.106298
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Consolidation-driven wrinkling in carbon/epoxy woven fabric prepregs: An experimental and numerical study

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Cited by 23 publications
(4 citation statements)
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“…6,7 Stacked UD prepregs are then conformed into the mold surface by the silicon diaphragm pulled by the vacuum. In HDF process, wrinkles are one of the most common defects 8,9 and are most likely to occur in the forming of doubly curved part or L shape part with large number of stacking plies, as shown in Figure 1. 10,11 Wrinkles not only affect the shape accuracy but also the strength of final composite part.…”
Section: Introductionmentioning
confidence: 99%
“…6,7 Stacked UD prepregs are then conformed into the mold surface by the silicon diaphragm pulled by the vacuum. In HDF process, wrinkles are one of the most common defects 8,9 and are most likely to occur in the forming of doubly curved part or L shape part with large number of stacking plies, as shown in Figure 1. 10,11 Wrinkles not only affect the shape accuracy but also the strength of final composite part.…”
Section: Introductionmentioning
confidence: 99%
“…Kulkarni et al [8] and Hassan [3] summarised numerous sources of fibre waviness. Some were inherent in the laminated composite: the stacking sequence [9,10], the difference of thermal expansion coefficients between the fibres and the matrix [11], the critical limb length [12], the inter-ply shear stress or the through-thickness compaction [13,14]. Other works have focused on the wrinkling sources in relation with the interactions between the part and the mould: the difference of thermal expansion coefficients [15,16], the proportion of 0 • plies and the size of the corner radius of the mould [17].…”
Section: Introductionmentioning
confidence: 99%
“…Both of these types of associated shrinkage are already taken into account for thin material. 15,[35][36][37][38][39][40][41][42][43] It was shown that the temperature field and thus the crystallization field are very sensitive to the thermal contact resistance (TCR). During the cooling in the consolidation process, deformation of the part, enhanced by thermal gradients, can create a contact loss between the surface of the part and the mold surface.…”
Section: Introductionmentioning
confidence: 99%