Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination

This paper presents the thermo-elastic effect on materials having anisotropic behavior and stresses developed due to residual temperature on interlaminar delamination fracture characteristics of composite skin stiffener. For the preexisting interlaminar delaminations subjected to uniaxial loading an...

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Main Authors: Saumya Shah, Pardeep Kumar, S.K. Panda, Sandeep Kumar
Format: Article
Language:English
Published: Elsevier 2019-11-01
Series:Journal of Materials Research and Technology
Online Access:http://www.sciencedirect.com/science/article/pii/S2238785419308968
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spelling doaj-235ceb8012a64ee1914e83d2014cbe112020-11-25T02:36:43ZengElsevierJournal of Materials Research and Technology2238-78542019-11-018659415949Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delaminationSaumya Shah0Pardeep Kumar1S.K. Panda2Sandeep Kumar3Department of Mechanical Engineering, MIET Meerut, IndiaDepartment of Mechanical Engineering, MIET Meerut, India; Corresponding author.Department of Mechanical Engineering, Indian Institute of Technology (B.H.U.), Varanasi, IndiaDepartment of Mechanical Engineering, MIET Meerut, IndiaThis paper presents the thermo-elastic effect on materials having anisotropic behavior and stresses developed due to residual temperature on interlaminar delamination fracture characteristics of composite skin stiffener. For the preexisting interlaminar delaminations subjected to uniaxial loading and three-point bending of three-dimensional coupled field thermo-elastic finite element analyses have been accomplished. The individual mode of strain energy release rate along the delamination front has been evaluated by modified crack-closure integral method based on the concept of mechanics of linear elastic fracture. Qualitative comparison has been illustrated for the individual modes of energy release rate along the delamination front of skin stiffener for both the loadings. The influence of coupled field thermo-elastic material anisotropy of the constituting laminae has been reasoned for the asymmetric variation of total strain energy release rate along delamination front. This was found to be significantly higher for the case of residual thermal stresses compared to mechanical loading. Keywords: Thermo-elastic effect, Interlaminar delamination, Crack closure, Energy release rate, Residual thermal stress.http://www.sciencedirect.com/science/article/pii/S2238785419308968
collection DOAJ
language English
format Article
sources DOAJ
author Saumya Shah
Pardeep Kumar
S.K. Panda
Sandeep Kumar
spellingShingle Saumya Shah
Pardeep Kumar
S.K. Panda
Sandeep Kumar
Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
Journal of Materials Research and Technology
author_facet Saumya Shah
Pardeep Kumar
S.K. Panda
Sandeep Kumar
author_sort Saumya Shah
title Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
title_short Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
title_full Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
title_fullStr Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
title_full_unstemmed Mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
title_sort mixed-mode thermo elastic delamination fracture behavior of composite skin stiffener containing interface delamination
publisher Elsevier
series Journal of Materials Research and Technology
issn 2238-7854
publishDate 2019-11-01
description This paper presents the thermo-elastic effect on materials having anisotropic behavior and stresses developed due to residual temperature on interlaminar delamination fracture characteristics of composite skin stiffener. For the preexisting interlaminar delaminations subjected to uniaxial loading and three-point bending of three-dimensional coupled field thermo-elastic finite element analyses have been accomplished. The individual mode of strain energy release rate along the delamination front has been evaluated by modified crack-closure integral method based on the concept of mechanics of linear elastic fracture. Qualitative comparison has been illustrated for the individual modes of energy release rate along the delamination front of skin stiffener for both the loadings. The influence of coupled field thermo-elastic material anisotropy of the constituting laminae has been reasoned for the asymmetric variation of total strain energy release rate along delamination front. This was found to be significantly higher for the case of residual thermal stresses compared to mechanical loading. Keywords: Thermo-elastic effect, Interlaminar delamination, Crack closure, Energy release rate, Residual thermal stress.
url http://www.sciencedirect.com/science/article/pii/S2238785419308968
work_keys_str_mv AT saumyashah mixedmodethermoelasticdelaminationfracturebehaviorofcompositeskinstiffenercontaininginterfacedelamination
AT pardeepkumar mixedmodethermoelasticdelaminationfracturebehaviorofcompositeskinstiffenercontaininginterfacedelamination
AT skpanda mixedmodethermoelasticdelaminationfracturebehaviorofcompositeskinstiffenercontaininginterfacedelamination
AT sandeepkumar mixedmodethermoelasticdelaminationfracturebehaviorofcompositeskinstiffenercontaininginterfacedelamination
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