2019
DOI: 10.1016/j.compstruct.2019.01.082
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Free vibration analysis of sandwich conical shells with fractional viscoelastic core

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Cited by 28 publications
(9 citation statements)
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“…Since the strength modulus of the viscoelastic layers are usually very small in comparison with the elastic layers, only the shear strain terms of the core layer are taken into account (Permoon et al, 2019). Moreover, the shear strains of the viscoelastic layer can be obtained as…”
Section: Governing Equations For Conical Shells 21 Model Definitionmentioning
confidence: 99%
See 3 more Smart Citations
“…Since the strength modulus of the viscoelastic layers are usually very small in comparison with the elastic layers, only the shear strain terms of the core layer are taken into account (Permoon et al, 2019). Moreover, the shear strains of the viscoelastic layer can be obtained as…”
Section: Governing Equations For Conical Shells 21 Model Definitionmentioning
confidence: 99%
“…Viscoelastic core layer. Using the fractional-order model for a viscoelastic layer, the shear stress-shear strain relations are expressed as (Permoon et al, 2019)…”
Section: Governing Equations For Conical Shells 21 Model Definitionmentioning
confidence: 99%
See 2 more Smart Citations
“…Rossikhin et al [31] studied the nonlinear vibrations of a fractionally damped cylindrical shell under the conditions of combinational internal resonance. Mokhtari et al [32,33] studied the vibration and aeroelastic flutter of sandwich cylindrical shells with fractionalorder viscoelastic core and isotropic face sheets, and Permoon et al [34] performed the same analysis for the vibration of sandwich conical shells with fractional core.…”
Section: Introductionmentioning
confidence: 99%