2015
DOI: 10.1016/j.ijmecsci.2014.11.020
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Fundamental frequency of the laminated composite cylindrical shell with clamped edges

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Cited by 15 publications
(6 citation statements)
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“…The solution of the bending problem for such a beam is presented by the authors in [23]. The similar approximation method was applied to the solution of the vibration problem for the laminated composite cylindrical shell with clamped edges [24]. Considering the above assumptions, the displacements, deflection and angles of rotation are approximated as follows:…”
Section: Solution Proceduresmentioning
confidence: 99%
“…The solution of the bending problem for such a beam is presented by the authors in [23]. The similar approximation method was applied to the solution of the vibration problem for the laminated composite cylindrical shell with clamped edges [24]. Considering the above assumptions, the displacements, deflection and angles of rotation are approximated as follows:…”
Section: Solution Proceduresmentioning
confidence: 99%
“…Sun et al [10] used Fourier series expansion method, which is derived by Stokes, transformation, to analyze the vibration characteristics of thin rotating cylindrical shells with several classical boundary conditions. Lopatin and Morozov [11] presented an analytical formula to calculate the fundamental frequencies for the laminated composite cylindrical shell with clamped edges based on the Fourier decomposition method. Wang et al [12] studied the vibration of a cantilever cylindrical shell suffered a moving harmonic excitation and the method of averaging was used to analyze the nonlinear traveling wave responses.…”
Section: Instructionmentioning
confidence: 99%
“…The result indicated that the different types of lay-up, properties of stiffeners, boundary conditions, and elastic foundation have significant effects on the fundamental frequency of laminated cylindrical shells. Lopatin and Morozov (2015), using Fourier and Galerkin methods, analyzed the free vibration of the laminated composite cylindrical shell with clamped edges. The result was calculated for various elastic and geometry parameters and compared with the finite element method.…”
Section: Introductionmentioning
confidence: 99%