2021
DOI: 10.1016/j.compstruct.2020.113533
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A couple stress model in non-polynomial framework to examine structural responses of laminated composite micro-plates: An analytical solution

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Cited by 8 publications
(3 citation statements)
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“…Soni et al [121] extended this framework to functionally graded, carbon-nanotube-reinforced plates, exploring static analysis. Joshan et al [122] introduced a coupled stress model within a non-polynomial framework to study the structural responses of laminated composite micro-plates, providing analytical solutions. Dhuria et al [123] examined the influence of porosity distribution on the static and buckling responses of porous, functionally graded plates, considering material heterogeneity.…”
Section: Thickness Functionsmentioning
confidence: 99%
“…Soni et al [121] extended this framework to functionally graded, carbon-nanotube-reinforced plates, exploring static analysis. Joshan et al [122] introduced a coupled stress model within a non-polynomial framework to study the structural responses of laminated composite micro-plates, providing analytical solutions. Dhuria et al [123] examined the influence of porosity distribution on the static and buckling responses of porous, functionally graded plates, considering material heterogeneity.…”
Section: Thickness Functionsmentioning
confidence: 99%
“…Also, the amplitude is highly affected by the shock pulse length factor, although decreasing the a/h, which is caused by reducing the b value, leads to an increase in the frequency and amplitude. In a further study, Joshan et al [301] employed the NPSDTs to perform an analytical investigation to explore the FV and the static responses of composite MSP. At the same time, the LSEs have been deliberated through implementing the CST, and various shear shape functions were considered to generate the TS deformation.…”
Section: Analytical Solution Without Considering the Sdementioning
confidence: 99%
“…[20][21][22][23][24][25][26][27][28][29][30][31] NPSDTs do not require shear correction factor and satisfy transverse shear free conditions at the top and bottom surface of the plate. 32 However, these theories are generally applied for modelling and analysis of plate structures of composites, sandwich and functionally graded materials. The modelling approaches of multilayered composite plates and shells considering their complicated effects are assessed by Giunta et al 33 Mirsky 34 evaluated the vibration response of thick laminated cylindrical shell using classical shell theory.…”
Section: Introductionmentioning
confidence: 99%