2023
DOI: 10.1007/s40430-023-04016-0
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Mathematical modeling and solution of nonlinear vibration problem of laminated plates with CNT originating layers interacting with two-parameter elastic foundation

Abstract: Generalizing the first-order shear deformation plate theory (FOPT) proposed by Ambartsumyan (Theory of anisotropic plates, Nauka, Moscow, 1967 (in Russian)) to the heterogeneous laminated nanocomposite plates and the nonlinear vibration problem is analytically solved taking into account an elastic medium in this study for the first time. The Pasternak-type elastic foundation model (PT-EF) is used as the elastic medium model. After creating the mathematical models of laminated rectangular plates with CNT origin… Show more

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Cited by 9 publications
(3 citation statements)
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References 41 publications
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“…The NL/linear vibrational period decreased due to increasing the amplitude. However, Avey et al [513] explored the NL FV responses of LCPs with CNT originating layers interacting with PF bases based on FSDT. Besides, the Galerkin approach was used to discretize NL ODEs which solved by semi-inverse methodology.…”
Section: Analytical Solution Without Considering the Sdementioning
confidence: 99%
“…The NL/linear vibrational period decreased due to increasing the amplitude. However, Avey et al [513] explored the NL FV responses of LCPs with CNT originating layers interacting with PF bases based on FSDT. Besides, the Galerkin approach was used to discretize NL ODEs which solved by semi-inverse methodology.…”
Section: Analytical Solution Without Considering the Sdementioning
confidence: 99%
“…30 Multiple researchers performed vibrational response estimation in the linear and nonlinear free and forced environments over various FG structures. [31][32][33][34][35] The skin panel of the airplane is where composite materials are most frequently employed when referring to the aerospace sector. This decision becomes much more critical when the aircraft is in a high-flight-dynamic condition because structural failure may be caused by aerodynamic heating.…”
Section: Introductionmentioning
confidence: 99%
“…Avey et al [ 39 ] presented the thermoelastic stability of CNT-patterned conical shells under thermal loading in the framework of FSDT. Avey et al [ 40 ] examined the mathematical modeling and solution of the nonlinear vibration problem of laminated plates with CNT-originating layers interacting with a two-parameter elastic foundation. Izadi et al [ 41 ] studied the bending characteristics of CNTs using micropolar elasticity models and MD simulations.…”
Section: Introductionmentioning
confidence: 99%