2012
DOI: 10.1002/zamm.201100173
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A numerical homogenisation method for sandwich plates based on a plate theory with thickness change

Abstract: Nowadays composite plates are widely used, especially in the transport industry. Their importance derives from their relatively low weight and good mechanical properties, but their behaviour is complex and cannot be obtained from a simple mixture rule properly. In the scope of this work, the considered composite plate is composed of a complex assembly of metal layers and carbon fibers reinforced polymers (CFRP) layers. Whereas the CFRP can be considered as anisotropic elastic, the metal layers have an elasto-p… Show more

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Cited by 21 publications
(11 citation statements)
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“…Towards a proper estimation of stresses in the unit cell, a coupling of global and local scales is required. In principle, approaches to scale coupling of plates or shells to 3D continua can be found in the literature, often referred to as FE 2 , see [47,48,49,50]. Common to these approaches is the use of FOSDT at global scale, which is not appropriate to solve structural problems for photovoltaic modules [9].However, these approaches have the objective to deliver effective material properties for the global scale.…”
Section: Projection Strategymentioning
confidence: 99%
“…Towards a proper estimation of stresses in the unit cell, a coupling of global and local scales is required. In principle, approaches to scale coupling of plates or shells to 3D continua can be found in the literature, often referred to as FE 2 , see [47,48,49,50]. Common to these approaches is the use of FOSDT at global scale, which is not appropriate to solve structural problems for photovoltaic modules [9].However, these approaches have the objective to deliver effective material properties for the global scale.…”
Section: Projection Strategymentioning
confidence: 99%
“…[16,17]. However, numerical techniques are required to estimate the effective transverse shear deformation in the inelastic range [18,19]. It should be mentioned that for laminates with extreme differences in the stiffness of layers the FSDT fails to predict the deformation properties of the laminate correctly, as shown for example in [4,7] for beams and in [20,21] for plates.…”
Section: Introductionmentioning
confidence: 97%
“…[4]. To estimate the effective transverse shear deformation in the inelastic range, various numerical techniques are available [16,17].…”
Section: Introductionmentioning
confidence: 99%