CV


FA
Mohammad Arefi

Mohammad Arefi

Professor

College: Faculty of Mechanical Engineering

Department: Mechanical Engineering - Solid Design

Degree: Ph.D

CV
FA
Mohammad Arefi

Professor Mohammad Arefi

College: Faculty of Mechanical Engineering - Department: Mechanical Engineering - Solid Design Degree: Ph.D |

Analysis of graphene nanoplatelet reinforced cylindrical shell subjected to thermo-mechanical loads

Authorsمحمد عارفی,سینا کیانی مقدم,الیاس محمدرضایی بیدگلی,مسعود کیانی,Omer Civalek
JournalCOMPOS STRUCT
Page number112924
Volume number255
IF5.407
Paper TypeFull Paper
Published At2021-01-01
Journal GradeScientific - research
Journal TypeElectronic
Journal CountryIran, Islamic Republic Of
Journal IndexJCR ,SCOPUS
KeywordsThermo‐elastic analysis Halpin‐Tsai model First‐order shear deformation theory Graphene nanoplatelets (GPLs) Functionally graded materials

Abstract

Analysis of graphene nanoplatelets (GPLs) reinforced cylindrical shell subjected to thermo‐mechanical loads is studied in this paper based on shear deformation theory. Halpin‐Tsai micromechanical model and rule of mix- tures are used for calculation of effective material properties of composite materials with different distributions of reinforcements including uniform symmetric and asymmetric distributions for nanoplatelet material. The various distributions are included UD (uniform distribution of GPLs along the thickness direction), FG‐O (linear variation of GPLs, where highest amount is locates at middle layer) and FG‐X(linear variation of GPLs, where highest amount is locates at top and bottom layers). The shear strains especially at both ends of cylindrical shell are included in our formulation using the two‐dimensional first‐order shear deformation theory (FSDT). Minimum total potential energy principle is used to derive the governing equations using Hooke’s law and application of Euler equations using the functional of the system. Eigenvalue and eigenvector method is used for solution of the governing equations. The radial and axial displacements and various com- ponents of stress are calculated in terms of number of layers, GPLs weight fraction, thermal loading, various distributions of reinforcement and coefficient of the elastic foundation. The numerical results indicate that maximum and minimum stresses are obtained for FG‐O and FG‐X distributions. Also, the biggest and lowest radial displacements are obtained for UD and FG‐X distributions, respectively.