2016
DOI: 10.1016/j.tws.2016.06.012
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A new nonlinear model for studying a sandwich panel with thin composite faces and elastic–plastic core

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Cited by 21 publications
(14 citation statements)
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“…The constitutive relationship of the component materials in the test joint is shown in Figure 5. To improve the accuracy and convergence speed of the finite-element analysis results, when the finite-element model is constructed, a fine meshing is used for the parts with holes and the parts where stress concentration can easily occur [25][26][27][28][29] (Figure 6). Additionally, to fully consider the contact between the upper and lower covers and the aluminum-alloy beams and the contact between the stainless-steel bolts and the bolt holes, face-to-face contact unit connections are used.…”
Section: Analysis Methodsmentioning
confidence: 99%
“…The constitutive relationship of the component materials in the test joint is shown in Figure 5. To improve the accuracy and convergence speed of the finite-element analysis results, when the finite-element model is constructed, a fine meshing is used for the parts with holes and the parts where stress concentration can easily occur [25][26][27][28][29] (Figure 6). Additionally, to fully consider the contact between the upper and lower covers and the aluminum-alloy beams and the contact between the stainless-steel bolts and the bolt holes, face-to-face contact unit connections are used.…”
Section: Analysis Methodsmentioning
confidence: 99%
“…Recently, numerical solutions have been explored by adopting the Ritz method based on EHSAPT or HSAPT. The accuracy of the Ritz method strongly depends on the choice of trial functions, including power series [13] or polynomial series [12]. These theoretical models seem relatively slow in convergence.…”
Section: Numerical Formulationmentioning
confidence: 99%
“…Rezaeifard et al. [12] presented a new nonlinear model for sandwich beams with transversely flexible cores based on HSAPT and derived the governing equations by Galerkin weighted residual method. As a progressive step, Salami et al.…”
Section: Introductionmentioning
confidence: 99%
“…Figure 4 shows the simplified constitutive relationships assumed for each part of the modeled specimen. The honeycomb core is modeled with shell elements while facesheets are modeled with solid elements [31][32][33]; core and facesheets are connected by contact elements [34,35]. As the model has symmetric geometrical dimensions, boundary constraint, and load, the analysis is based on a semi-structure, unidirectional, and uniform displacement load is applied to the end surface of the honeycomb sandwich structure at the slip end.…”
Section: Finite Element Modeling and Analysismentioning
confidence: 99%