2020
DOI: 10.1016/j.compstruct.2020.112631
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Experimental and numerical analysis of novel multi-layer sandwich panels under three point bending load

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Cited by 61 publications
(26 citation statements)
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“…The shear stress has the largest effect on the core tearing during the three-point bending test [ 11 , 29 , 30 ]. The shear strength of ABS is taken as half of the yielding stress.…”
Section: Resultsmentioning
confidence: 99%
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“…The shear stress has the largest effect on the core tearing during the three-point bending test [ 11 , 29 , 30 ]. The shear strength of ABS is taken as half of the yielding stress.…”
Section: Resultsmentioning
confidence: 99%
“…TPMSs under compressive loading and sandwich beams with a 3D truss cell/foam core under three-point bending have been studied extensively [ 29 , 30 , 31 , 32 ]. In this study, the objective was to compare the total deformation and stress distribution of SPSs containing TPMS lattice cores with different relative densities.…”
Section: Introductionmentioning
confidence: 99%
“…Energy absorption is key to testing the structural integrity in the event of failure. As shown in some articles (Jin et al 2015;Yan et al 2014;Schneider et al 2016;Sun et al 2017;Yazdani Sarvestani et al 2018;Smardzewski 2019b;Ha and Lu 2020;Farrokhabadi et al 2020), the honeycomb panels exhibit excellent energy absorption properties. The energy absorption E a (J) of the selected panels was calculated as follows: where SE a (J) is specific energy absorption, m is the mass of the energy absorber.…”
Section: Methodsmentioning
confidence: 95%
“…They demonstrated that the defects acted as potential areas for crack development and observed that the presence of imperfections in the sample might have a more beneficial impact on the toughness than on the strength as long as the distance between imperfections is short enough. Investigation of failure in the micromechanical mode will lead to a better understanding of failure at the macromechanical scale, hence to analyze the failure at the macromechanical scale in composites by examining the failure at the failure sites need to magnify and examine each model 20,21 . For this reason, general failures at the micromechanical scale should be recognized.…”
Section: Introductionmentioning
confidence: 99%