2021
DOI: 10.1177/10996362211020388
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Optimization of dynamic properties for laminated multiphase nanocomposite sandwich conical shell in thermal and magnetic conditions

Abstract: This paper extends an optimization procedure to obtain the optimal dynamic properties of laminated sandwich multiphase nanocomposite truncated conical shell under magneto-hygro-thermal conditions. Based on principle of Hamilton, the equations of motion are obtained and solved by differential quadrature method and Bolotin's methods for obtaining the dynamic stability region. Based on particle swarm optimization and harmony search algorithms, a novel hybrid optimization method basis HS and PSO is proposed to enh… Show more

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Cited by 46 publications
(6 citation statements)
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“…In this work, in order to solve the motion equations and determine the dynamic instability region (DIR), DQM is employed. Hence, different order of differential equations of cylindrical shell can be converted to set of algebraic equations using following relations 21–32 dnF(),xiθjitalicdxngoodbreak=k=1NxAiknF(),xkθj2.639999emngoodbreak=1,,Nxgoodbreak−1, dmF(),xiθjdθmgoodbreak=l=1NθBjlmF(),xiθl2.52emmgoodbreak=1,,Nθgoodbreak−1, dn+mF(),xiθjdxndθmgoodbreak=k=1Nxl=1NθAiknBjlmF(),xkθl, in which Aikn as well as Bjlm define weighting coefficients and are expressed as A…”
Section: Solving Proceduresmentioning
confidence: 99%
“…In this work, in order to solve the motion equations and determine the dynamic instability region (DIR), DQM is employed. Hence, different order of differential equations of cylindrical shell can be converted to set of algebraic equations using following relations 21–32 dnF(),xiθjitalicdxngoodbreak=k=1NxAiknF(),xkθj2.639999emngoodbreak=1,,Nxgoodbreak−1, dmF(),xiθjdθmgoodbreak=l=1NθBjlmF(),xiθl2.52emmgoodbreak=1,,Nθgoodbreak−1, dn+mF(),xiθjdxndθmgoodbreak=k=1Nxl=1NθAiknBjlmF(),xkθl, in which Aikn as well as Bjlm define weighting coefficients and are expressed as A…”
Section: Solving Proceduresmentioning
confidence: 99%
“…Advanced composite materials possess the advantages of high specific strength and modulus. [1,2] Thus, they are ideal materials for modern aerospace applications, such as airplanes, rockets, satellites, and spacecraft. The designability of composite materials provides a broad space for further improvements to their mechanical properties and structural optimization.…”
Section: Introductionmentioning
confidence: 99%
“…Because of its advantageous features, such as high damping capacity, high specific strength, and high specific rigidity, composite sandwich structures constituted by two hard face layers and a soft core have been widely used in rail transport, aerospace applications, and other industries. [1][2][3] Therefore, the study of free vibration and damping property of circular composite sandwich cylindrical shells (CCSCS) has important research value.…”
Section: Introductionmentioning
confidence: 99%