2015
DOI: 10.1016/j.compositesb.2015.03.025
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Multiobjective design of viscoelastic laminated composite sandwich panels

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Cited by 69 publications
(26 citation statements)
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“…Two objectives were considered: (i) to maximize the local-global buckling strength and (ii) to maximize the distortional buckling strength. This bi-objective optimization problem was solved using the Direct MultiSearch (DMS [9,10]) method, which does not use any derivatives of the objective functions. Like in previous studies available in the literature, the design variables of the problem were the angles of orientation of cross-section wall elements.…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…Two objectives were considered: (i) to maximize the local-global buckling strength and (ii) to maximize the distortional buckling strength. This bi-objective optimization problem was solved using the Direct MultiSearch (DMS [9,10]) method, which does not use any derivatives of the objective functions. Like in previous studies available in the literature, the design variables of the problem were the angles of orientation of cross-section wall elements.…”
Section: Discussionmentioning
confidence: 99%
“…It is based on a novel technique developed by extending direct search from single to multiobjective optimization. DMS has recently been used for the design of a viscoelastic laminated sandwich composite panels [10], thus maximizing modal damping and minimum mass and material cost, by choosing the number of layers, the material of the layers, as well as the respective thickness and orientation. Very recently, Yin et al [11] also used multiobjective optimization to maximize the specific energy absorption and minimize the maximum impact force of foam-filled multi-cell thin-walled structure using nonlinear finite element method and multiobjective particle swarm optimization algorithm.…”
Section: Introductionmentioning
confidence: 99%
“…For the core viscoelastic material and assuming that Young's modulus and Poisson's ratio depend on the frequency [8,24] one can write them according to * = (1 + ) ,…”
Section: Constitutive Relationsmentioning
confidence: 99%
“…Many optimization techniques such as Genetic Algorithm 14 , Moving Asymptotes method 15 , Topology Optimization method 16 , modal strain energy method 17 and recently Double Shear Lap-Joint-configuration 13,18 were successfully adopted to optimize the location and dimensions of CLD, in order to maximize the structural damping while minimizing additional mass. However, the introducing of the damping layer can reduce the stiffness of the sandwich structures 11 .…”
Section: Introductionmentioning
confidence: 99%