2015
DOI: 10.5755/j01.mech.21.2.10276
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Modeling of constitutive behavior of anisotropic composite material using multi-scale approach

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Cited by 5 publications
(4 citation statements)
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“…The homogenization problem consists in the determination of effective material constants of a heterogeneous material [22,36]. The material constants are involved in the relation between macro (averaged) stresses and strains:…”
Section: Numerical Homogenization Of Structures With Spherical Cavitiesmentioning
confidence: 99%
“…The homogenization problem consists in the determination of effective material constants of a heterogeneous material [22,36]. The material constants are involved in the relation between macro (averaged) stresses and strains:…”
Section: Numerical Homogenization Of Structures With Spherical Cavitiesmentioning
confidence: 99%
“…The stiffness of multi-phase material can be estimated with the help of various approaches that have already been proposed. One of the most versatile method that can deal with the finite number of phases of any morphology is numerical homogenization based on finite [8][9][10] or boundary [11,12] element analysis of representative volume element (RVE). On the other hand, this approach generally requires relatively high computational cost.…”
Section: Effective Stiffness Of Three Phase Materialsmentioning
confidence: 99%
“…Finite element based homogenization was performed for representative volume element containing three phases (similar to the one presented in Fig. 1) in a way presented in the previous works of authors [8,9]. It should be underlined that, in general, the applicability of multi-phase Mori-Tanaka methods is limited by their tendency to predict non-symmetric stiffness tensors.…”
Section: Fig 1 Multi Level Homogenization Scheme Using the Example Omentioning
confidence: 99%
“…The problem of optimal design of the wing as well for passenger or military aircraft, as for Unmanned Aerial Vehicle (UAV), has been considered by many researchers [3][4][5]. Different methods (bio-inspired techniques or gradient based algorithms) have been used for single and multiobjective optimization, only for properties of the composite materials [6][7][8][9][10], as well as for properties of entire components [11,12]. The paper presents an application of the inhouse implementation of the evolutionary multi-objective algorithm in optimization of the UAV wing part.…”
Section: Introductionmentioning
confidence: 99%