2021
DOI: 10.1016/j.coco.2021.100878
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Enhancing strength and stiffness of composite joint through co-cure technique

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Cited by 30 publications
(15 citation statements)
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“…The frequency response and damping value of composites were calculated directly using DEWE tools. Using the circle fit method, DEWE software measures damping value related to a specific mode with the following expression (1).…”
Section: Experimental Free Vibrational Analysismentioning
confidence: 99%
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“…The frequency response and damping value of composites were calculated directly using DEWE tools. Using the circle fit method, DEWE software measures damping value related to a specific mode with the following expression (1).…”
Section: Experimental Free Vibrational Analysismentioning
confidence: 99%
“…Composite joints can be secondary bonded, which requires the adhesive joining of two cured laminates, or co‐bonded, which requires adhesive joining of uncured laminate with cured laminate or co‐cured, which requires the curing of both the laminates and the adhesive in a single production process. [ 23 ] Before using these materials in critical load‐bearing applications, a better understanding of the failure behavior of these composite joining methods is necessary. Co‐cure joints, for instance, can have issues with entombed water, both free and bound have been released during the joining process, adversely impacting the adhesive joint's performance.…”
Section: Introductionmentioning
confidence: 99%
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“…Thus, it caused composite adherend to bend out-of-plane and increased the transverse peel stress in the adhesive layer, which initiated the crack formation and reduced failure resistance of composite joints. 11,12 Researchers developed three-dimensional reinforcement methods such as braiding, stitching, tufting, weaving and Zpinning to enhance the reliability and structural efficacy of the composite joints. 13,14 Z-pinning is an effective method to enhance composite joints' shear properties and fatigue life.…”
Section: Introductionmentioning
confidence: 99%
“…Thus, it caused composite adherend to bend out-of-plane and increased the transverse peel stress in the adhesive layer, which initiated the crack formation and reduced failure resistance of composite joints. 11,12…”
Section: Introductionmentioning
confidence: 99%