Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading

Elastoplastic analysis of a composite cylinder, consisting of an isotropic elastic inclusion surrounded by orthotropic matrix, is conducted via numerical parametric studies for examining its residual stress under thermal cycles. The matrix is assumed to be elastically and plastically orthotropic, an...

Full description

Bibliographic Details
Main Authors: Somayeh Bagherinejad Zarandi, Hsiang-Wei Lai, Yun-Che Wang, Sergey Aizikovich
Format: Article
Language:English
Published: MDPI AG 2019-03-01
Series:Symmetry
Subjects:
Online Access:http://www.mdpi.com/2073-8994/11/3/320
id doaj-ade2a7e0b8664f0788fe50d4440fc315
record_format Article
spelling doaj-ade2a7e0b8664f0788fe50d4440fc3152020-11-24T21:16:05ZengMDPI AGSymmetry2073-89942019-03-0111332010.3390/sym11030320sym11030320Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and UnloadingSomayeh Bagherinejad Zarandi0Hsiang-Wei Lai1Yun-Che Wang2Sergey Aizikovich3Department of Civil Engineering, National Cheng Kung University, Tainan 70101, TaiwanDepartment of Civil Engineering, National Cheng Kung University, Tainan 70101, TaiwanDepartment of Civil Engineering, National Cheng Kung University, Tainan 70101, TaiwanResearch and Education Center “Materials”, Don State Technical University, Rostov-on-Don 344000, RussiaElastoplastic analysis of a composite cylinder, consisting of an isotropic elastic inclusion surrounded by orthotropic matrix, is conducted via numerical parametric studies for examining its residual stress under thermal cycles. The matrix is assumed to be elastically and plastically orthotropic, and all of its material properties are temperature-dependent (TD). The Hill’s anisotropic plasticity material model is adopted. The interface between the inclusion and matrix is perfectly bonded, and the outer boundary of the cylinder is fully constrained. A quasi-static, uniform temperature field is applied to the cylinder, which is analyzed under the plane-strain assumption. The mechanical responses of the composite cylinder are strongly affected by the material symmetry and temperature-dependent material properties. When the temperature-independent material properties are assumed, larger internal stresses at the loading phase are predicted. Furthermore, considering only yield stress being temperature dependent may be insufficient since other TD material parameters may also affect the stress distributions. In addition, plastic orthotropy inducing preferential yielding along certain directions leads to complex residual stress distributions when material properties are temperature-dependent.http://www.mdpi.com/2073-8994/11/3/320orthotropic plasticityresidual stresstemperature-dependent material propertiescomposite cylinderfinite element analysis
collection DOAJ
language English
format Article
sources DOAJ
author Somayeh Bagherinejad Zarandi
Hsiang-Wei Lai
Yun-Che Wang
Sergey Aizikovich
spellingShingle Somayeh Bagherinejad Zarandi
Hsiang-Wei Lai
Yun-Che Wang
Sergey Aizikovich
Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
Symmetry
orthotropic plasticity
residual stress
temperature-dependent material properties
composite cylinder
finite element analysis
author_facet Somayeh Bagherinejad Zarandi
Hsiang-Wei Lai
Yun-Che Wang
Sergey Aizikovich
author_sort Somayeh Bagherinejad Zarandi
title Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
title_short Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
title_full Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
title_fullStr Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
title_full_unstemmed Residual Stress Analysis of an Orthotropic Composite Cylinder under Thermal Loading and Unloading
title_sort residual stress analysis of an orthotropic composite cylinder under thermal loading and unloading
publisher MDPI AG
series Symmetry
issn 2073-8994
publishDate 2019-03-01
description Elastoplastic analysis of a composite cylinder, consisting of an isotropic elastic inclusion surrounded by orthotropic matrix, is conducted via numerical parametric studies for examining its residual stress under thermal cycles. The matrix is assumed to be elastically and plastically orthotropic, and all of its material properties are temperature-dependent (TD). The Hill’s anisotropic plasticity material model is adopted. The interface between the inclusion and matrix is perfectly bonded, and the outer boundary of the cylinder is fully constrained. A quasi-static, uniform temperature field is applied to the cylinder, which is analyzed under the plane-strain assumption. The mechanical responses of the composite cylinder are strongly affected by the material symmetry and temperature-dependent material properties. When the temperature-independent material properties are assumed, larger internal stresses at the loading phase are predicted. Furthermore, considering only yield stress being temperature dependent may be insufficient since other TD material parameters may also affect the stress distributions. In addition, plastic orthotropy inducing preferential yielding along certain directions leads to complex residual stress distributions when material properties are temperature-dependent.
topic orthotropic plasticity
residual stress
temperature-dependent material properties
composite cylinder
finite element analysis
url http://www.mdpi.com/2073-8994/11/3/320
work_keys_str_mv AT somayehbagherinejadzarandi residualstressanalysisofanorthotropiccompositecylinderunderthermalloadingandunloading
AT hsiangweilai residualstressanalysisofanorthotropiccompositecylinderunderthermalloadingandunloading
AT yunchewang residualstressanalysisofanorthotropiccompositecylinderunderthermalloadingandunloading
AT sergeyaizikovich residualstressanalysisofanorthotropiccompositecylinderunderthermalloadingandunloading
_version_ 1726017192427782144