2018
DOI: 10.1016/j.ijadhadh.2018.06.003
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Fatigue crack propagation rate of CFRP/aluminum adhesively bonded DCB joints with acrylic and epoxy adhesives

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Cited by 17 publications
(5 citation statements)
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“…Imanaka et al [105] evaluated the influence of the thickness ratio of the dissimilar double cantilever beam with acrylic and epoxy adhesives on the fatigue crack growth rate. The ratio of the thickness of the lower adherend to the upper adherend is a vital factor in determining the mode ratio 𝐺𝐺 𝐼𝐼𝐼𝐼 /𝐺𝐺 𝐼𝐼 (where 𝐺𝐺 𝐼𝐼 and 𝐺𝐺 𝐼𝐼𝐼𝐼 are strain energy release rate in mode I and II, respectively) and the stress distribution at the crack-tip.…”
Section: Adherends and Adhesive Thickness And Lengthmentioning
confidence: 99%
“…Imanaka et al [105] evaluated the influence of the thickness ratio of the dissimilar double cantilever beam with acrylic and epoxy adhesives on the fatigue crack growth rate. The ratio of the thickness of the lower adherend to the upper adherend is a vital factor in determining the mode ratio 𝐺𝐺 𝐼𝐼𝐼𝐼 /𝐺𝐺 𝐼𝐼 (where 𝐺𝐺 𝐼𝐼 and 𝐺𝐺 𝐼𝐼𝐼𝐼 are strain energy release rate in mode I and II, respectively) and the stress distribution at the crack-tip.…”
Section: Adherends and Adhesive Thickness And Lengthmentioning
confidence: 99%
“…Because large structures are always subject to periodic loads, fatigue performance of structural acrylic adhesives is important. Therefore, the effects of substrate thickness, 34 substrate materials, 35 adhesive thickness, 36 mode mixity, 37 and R-ratio 36,38 on the FCG behavior have been discussed for structural acrylic adhesives. However, research on this topic is scarce compared to epoxy adhesives, and further understanding will significantly help in predicting the fatigue life of joints more accurately.…”
Section: Introductionmentioning
confidence: 99%
“…Yang [ 25 ] studied the fatigue performance of CFRP-steel adhesive joints under cyclic shear loading through experiments. Imanaka [ 26 ] studied the fatigue crack growth of CFRP-Al (Aluminium) DCB test specimens. Sellitto [ 27 ] numerically investigated the stringer termination delamination in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel with VCCT.…”
Section: Introductionmentioning
confidence: 99%