2021
DOI: 10.1177/1081286520978488
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A non-classical model for first-ordershear deformation circular cylindrical thin shells incorporating microstructure and surface energy effects

Abstract: A new non-classical model for first-order shear deformation circular cylindrical thin shells is developed by using a modified couple stress theory and a surface elasticity theory. Through a variational formulation based on Hamilton’s principle, the equations of motion and boundary conditions are simultaneously obtained, and the microstructure and surface energy effects are treated in a unified manner. The newly developed non-classical shell model contains one material length-scale parameter to account for the m… Show more

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Cited by 18 publications
(6 citation statements)
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“…are the Cauchy stress resultants through the shell thickness. The kinetic energy of the shell has the form [25,26]:…”
Section: Orthotropic Cylindrical Shell Model With the Rotary Inertia ...mentioning
confidence: 99%
“…are the Cauchy stress resultants through the shell thickness. The kinetic energy of the shell has the form [25,26]:…”
Section: Orthotropic Cylindrical Shell Model With the Rotary Inertia ...mentioning
confidence: 99%
“…The size effect induces distinct mechanical properties in microstructures compared to macrostructures. Currently, many high-order theories are proposed to describe the size effect [35][36][37][38][39][40][41][42][43][44], such as the couple stress theory [45], strain gradient theory [46], non-local elasticity theory [47], surface elasticity theory [48], and reformulated strain gradient elasticity theory [49][50][51]. Utilizing the couple stress theory, Yang et al established the modified couple stress theory (MCST), which specifically accounts for the symmetric curvature tensor with one additional material parameter for isotropic material.…”
Section: Model and Formulationmentioning
confidence: 99%
“…where u x , u θ and u z are, respectively, the x-, θ -and z-components of the displacement vector u of a point (x, θ , z) in the shell at time t, and u and w are, respectively, the x-and z-displacement components of the corresponding point (x, θ , 0) on the shell middle surface at time t. Note that u θ is identically zero and there is no dependence on θ for all kinematic and kinetic quantities in such an axisymmetric problem (e.g., [11,14]), which differ from those in general deformations of circular cylindrical shells (e.g., [37,40]). From Eq.…”
Section: Axisymmetric Circular Cylindrical Shell Model With the Rotar...mentioning
confidence: 99%