2015
DOI: 10.1016/j.compstruct.2014.10.020
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Experimental study on the fatigue behaviour of honeycomb sandwich panels with artificial defects

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Cited by 60 publications
(18 citation statements)
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“…Abbadi et al investigated the fatigue behaviors of undamaged and damaged specimens by using four-point bending loads. The results obtained indicated that the damage formed had no effect on the static strength of specimens 19 . Schubel et al stated that difficult-to-detect damage like delamination formed in sandwich composites after impact caused significant reductions in the strength of specimens 20 .…”
Section: Introductionmentioning
confidence: 90%
“…Abbadi et al investigated the fatigue behaviors of undamaged and damaged specimens by using four-point bending loads. The results obtained indicated that the damage formed had no effect on the static strength of specimens 19 . Schubel et al stated that difficult-to-detect damage like delamination formed in sandwich composites after impact caused significant reductions in the strength of specimens 20 .…”
Section: Introductionmentioning
confidence: 90%
“…Density (kg/m 3 ) E/q (Nm/kg) r/q (Nm/kg) C/q (Nm/kg) two types of defects: Brinell balls and Drilling holes were investigated [59]. The data also compare aluminum and aramid fibers under fatigue loading.…”
Section: Material Cell Size (Mm)mentioning
confidence: 99%
“…On the other hand, many efforts have been made to experimentally or numerically study the fatigue behavior of sandwich panels with face/core interfacial cracks 1118 , core cracks 19 , inserts 20 , face wrinkle defects 21 , artificial defect 22 , or weld notches 23 . Moreover, the influences of some loading variables, such as variable amplitudes of cyclic loading 24–25 , load ratios 2627 , load frequencies 28 and low-velocity impact 29 on the fatigue strength of sandwich structures have been also investigated.…”
Section: Introductionmentioning
confidence: 99%