2017
DOI: 10.1080/15376494.2017.1341583
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Nonlinear buckling and postbuckling of imperfect piezoelectric S-FGM circular cylindrical shells with metal–ceramic–metal layers in thermal environment using Reddy's third-order shear deformation shell theory

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Cited by 75 publications
(16 citation statements)
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“…Properties of the FGM media are obtained according to the simple rule of mixtures, same as Equation . Here T=T0+ΔT, and ΔT is the temperature rise from reference temperature T 0 at room temperature (300K).…”
Section: Resultsmentioning
confidence: 99%
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“…Properties of the FGM media are obtained according to the simple rule of mixtures, same as Equation . Here T=T0+ΔT, and ΔT is the temperature rise from reference temperature T 0 at room temperature (300K).…”
Section: Resultsmentioning
confidence: 99%
“…In this study, except for Poisson's ratio which is assumed to be constant, the other temperature-dependent functionally graded material properties are assumed to be nonlinear functions of temperature and may be expressed by the following function [35,36] ( ) = 0 ( . [37][38][39][40][41][42][43][44][45][46][47][48][49][50] Here = 0 + Δ , and Δ is the temperature rise from reference temperature 0 at room temperature (300K). Also, ( = 0, ±1, 2, 3) are temperature-dependent coefficients of the FG material properties given by Table. 1.…”
Section: Resultsmentioning
confidence: 99%
“…Khoa et al. [22] used the TSDT for buckling and post buckling analysis of a cylindrical shell. It is subjected to the external pressure, axial pressure, and electrical load.…”
Section: Introductionmentioning
confidence: 99%
“…Each model allows a vast range of analysis, and according to the type of the studied structure (thin, moderately thick or thick) and its applicability domain (linear, nonlinear, static, dynamic, free vibration, buckling or postbuckling), one can choose the appropriate model to assess the desired investigation. The detailed information on these models can be found in the literature [10,44,54,58,62,68]. The accuracy and computational costs of such models are still a great concern for many researchers, especially if the shell structure undergoes large displacements and finite rotations.…”
Section: Introductionmentioning
confidence: 99%