2015
DOI: 10.1016/j.compstruct.2015.04.017
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A unified method for the vibration and damping analysis of constrained layer damping cylindrical shells with arbitrary boundary conditions

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Cited by 64 publications
(23 citation statements)
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“…The boundaries of the elastically restrained shell are described by setting the values of translational springs and rotational spring, and the boundaries of cylindrical shells can be stated as follows (Jin et al, 2015;Jin et al, 2013):…”
Section: The Boundary Conditions At the Edgesmentioning
confidence: 99%
“…The boundaries of the elastically restrained shell are described by setting the values of translational springs and rotational spring, and the boundaries of cylindrical shells can be stated as follows (Jin et al, 2015;Jin et al, 2013):…”
Section: The Boundary Conditions At the Edgesmentioning
confidence: 99%
“…And at each point the restraint condition is represented as four sets of independent springs, including three sets of linear springs and one set of rotational springs, and different boundary conditions can be obtained by setting different spring stiffness. Jin et al [18][19][20] developed a series of methods to investigate free vibration of different cylindrical shells with general elastically restrained boundaries, such as composite laminated cylindrical shells and a three-layered passive constrained layer damping (PCLD) cylindrical shell, considering elastic restraints and intermediate ring supports. Qu et al [21] applied the method of domain decomposition to the analysis of cylindrical shells.…”
Section: Instructionmentioning
confidence: 99%
“…Based on the excellent convergence obtained from the modified Fourier series method together with Ritz method, it is widely used in various studies on vibrations of functionally graded circular, annular and sector plates and curved shells involving various complex boundary conditions [22][23][24][25][26][27][28][29][30].…”
Section: Introductionmentioning
confidence: 99%