2022
DOI: 10.1007/s11071-022-07811-x
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Nonlinear forced vibration of hybrid fiber/graphene nanoplatelets/polymer composite sandwich cylindrical shells with hexagon honeycomb core

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Cited by 19 publications
(2 citation statements)
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“…Gupta and Pradyumna [27] adopted the thirdorder shear deformation theory considering the Murakami zig-zag effects to analyze the geometric nonlinear dynamic behaviors of sandwich shell panels with an auxetic core and fiber reinforced skins, and the authors also examined the feasibility of the composite auxetic core with variable stiffness characteristics. Dong et al [28] proposed an advanced cylindrical shell with three phase hybrid composite material skins and a hexagon honeycomb core, and investigated the nonlinear forced vibration responses of the structure in hygrothermal environments using the material homogenization approach, FSDT combined with von Ka´rma´n nonlinearity terms, and the multiple scale method. According to RHSDT incorporating von Karman's nonlinear theory, Karimiasl and Alibeigloo [29] employed the differential quadrature method and homotopy technique to solve the nonlinear free vibration properties of sandwich shell panels with a double U auxetic core and FG skins.…”
Section: Introductionmentioning
confidence: 99%
“…Gupta and Pradyumna [27] adopted the thirdorder shear deformation theory considering the Murakami zig-zag effects to analyze the geometric nonlinear dynamic behaviors of sandwich shell panels with an auxetic core and fiber reinforced skins, and the authors also examined the feasibility of the composite auxetic core with variable stiffness characteristics. Dong et al [28] proposed an advanced cylindrical shell with three phase hybrid composite material skins and a hexagon honeycomb core, and investigated the nonlinear forced vibration responses of the structure in hygrothermal environments using the material homogenization approach, FSDT combined with von Ka´rma´n nonlinearity terms, and the multiple scale method. According to RHSDT incorporating von Karman's nonlinear theory, Karimiasl and Alibeigloo [29] employed the differential quadrature method and homotopy technique to solve the nonlinear free vibration properties of sandwich shell panels with a double U auxetic core and FG skins.…”
Section: Introductionmentioning
confidence: 99%
“…Some scholars utilized Ritz method and Gram-Schmidt polynomials to form approximate functions and analyzed the free vibration of RCS [19]. Furthermore, some scholars studied the nonlinear vibration of cylindrical shells of composite materials [20][21][22][23][24].…”
Section: Introductionmentioning
confidence: 99%