Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations
Nonlinear thermo-elastic buckling characteristics of composite variable stiffness beam with layers making use of curvilinear fibres under thermal environment is attempted here. The model is based on a shear deformable theory introducing trigonometric function, and considering von Kármán’s assumption...
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Veröffentlicht in: | International journal of non-linear mechanics 2023-01, Vol.148, p.104303, Article 104303 |
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creator | Manickam, Ganapathi Haboussi, Mohamed D’Ottavio, Michele Kulkarni, Vedang Chettiar, Alfred Gunasekaran, Vijay |
description | Nonlinear thermo-elastic buckling characteristics of composite variable stiffness beam with layers making use of curvilinear fibres under thermal environment is attempted here. The model is based on a shear deformable theory introducing trigonometric function, and considering von Kármán’s assumptions based geometrical nonlinear effect. The beam constitutive equation is modified according to the stress-free situation in the width direction of beam-Poisson’s effect in the formulation for predicting the behaviour of general lay-up composite beams. By the principle of minimum total potential energy, the governing equations in terms of incremental stiffness matrices are formed introducing general beam finite element. The global equilibrium equations formulated are solved for envisaging the post-buckling path through eigenvalue analysis iteratively, thus establishing the relationship of thermal temperature against moderate amplitude level of beam deflection. A systematic parametric analysis considering different lamina properties such as curvilinear fibre path angles and including lay-up sequences, thermal expansion coefficient, mixed laminate combining straight and curvilinear fibres-based layers is carried out on thermo-structural stability of curvilinear fibre-based beams. Also, the influence of geometric factors, flexible beam end support, and variation in thermal profile, etc. over the stability behaviour of beam is examined.
•Studied the nonlinear thermo-elastic stability of general lay-up composite beams using modified constitutive equations.•Established the nonlinear thermal elastic stability region of composite beams including the effects of curvilinear fibres.•Predicted the temperature rise after buckling against beam deflection, exhibiting varied hard spring type behaviour.•Confirmed the beam equilibrium state change associated with the instability in the nonlinear region.•Wide range of parametric analysis made here form benchmark solutions for other analytical/numerical models. |
doi_str_mv | 10.1016/j.ijnonlinmec.2022.104303 |
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•Studied the nonlinear thermo-elastic stability of general lay-up composite beams using modified constitutive equations.•Established the nonlinear thermal elastic stability region of composite beams including the effects of curvilinear fibres.•Predicted the temperature rise after buckling against beam deflection, exhibiting varied hard spring type behaviour.•Confirmed the beam equilibrium state change associated with the instability in the nonlinear region.•Wide range of parametric analysis made here form benchmark solutions for other analytical/numerical models.</description><identifier>ISSN: 0020-7462</identifier><identifier>EISSN: 1878-5638</identifier><identifier>DOI: 10.1016/j.ijnonlinmec.2022.104303</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Beam deflection ; Curvilinear fibre angles ; Engineering Sciences ; Mechanics ; Nonlinear thermo-elastic stability ; Rotational spring ; Structural mechanics ; Thermal buckling ; Thermal temperature rise ; Variable stiffness composite beams</subject><ispartof>International journal of non-linear mechanics, 2023-01, Vol.148, p.104303, Article 104303</ispartof><rights>2022</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c285t-38fbe7e01b7585f66976ef106ad2e8b61b2c4cbcde68f597b8f79bb7b0f673633</citedby><cites>FETCH-LOGICAL-c285t-38fbe7e01b7585f66976ef106ad2e8b61b2c4cbcde68f597b8f79bb7b0f673633</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.ijnonlinmec.2022.104303$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>230,314,780,784,885,3550,27924,27925,45995</link.rule.ids><backlink>$$Uhttps://hal.parisnanterre.fr/hal-04325282$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Manickam, Ganapathi</creatorcontrib><creatorcontrib>Haboussi, Mohamed</creatorcontrib><creatorcontrib>D’Ottavio, Michele</creatorcontrib><creatorcontrib>Kulkarni, Vedang</creatorcontrib><creatorcontrib>Chettiar, Alfred</creatorcontrib><creatorcontrib>Gunasekaran, Vijay</creatorcontrib><title>Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations</title><title>International journal of non-linear mechanics</title><description>Nonlinear thermo-elastic buckling characteristics of composite variable stiffness beam with layers making use of curvilinear fibres under thermal environment is attempted here. The model is based on a shear deformable theory introducing trigonometric function, and considering von Kármán’s assumptions based geometrical nonlinear effect. The beam constitutive equation is modified according to the stress-free situation in the width direction of beam-Poisson’s effect in the formulation for predicting the behaviour of general lay-up composite beams. By the principle of minimum total potential energy, the governing equations in terms of incremental stiffness matrices are formed introducing general beam finite element. The global equilibrium equations formulated are solved for envisaging the post-buckling path through eigenvalue analysis iteratively, thus establishing the relationship of thermal temperature against moderate amplitude level of beam deflection. A systematic parametric analysis considering different lamina properties such as curvilinear fibre path angles and including lay-up sequences, thermal expansion coefficient, mixed laminate combining straight and curvilinear fibres-based layers is carried out on thermo-structural stability of curvilinear fibre-based beams. Also, the influence of geometric factors, flexible beam end support, and variation in thermal profile, etc. over the stability behaviour of beam is examined.
•Studied the nonlinear thermo-elastic stability of general lay-up composite beams using modified constitutive equations.•Established the nonlinear thermal elastic stability region of composite beams including the effects of curvilinear fibres.•Predicted the temperature rise after buckling against beam deflection, exhibiting varied hard spring type behaviour.•Confirmed the beam equilibrium state change associated with the instability in the nonlinear region.•Wide range of parametric analysis made here form benchmark solutions for other analytical/numerical models.</description><subject>Beam deflection</subject><subject>Curvilinear fibre angles</subject><subject>Engineering Sciences</subject><subject>Mechanics</subject><subject>Nonlinear thermo-elastic stability</subject><subject>Rotational spring</subject><subject>Structural mechanics</subject><subject>Thermal buckling</subject><subject>Thermal temperature rise</subject><subject>Variable stiffness composite beams</subject><issn>0020-7462</issn><issn>1878-5638</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNqNkUGvEyEUhYnRxPr0P-DSxVRgOkCXL436TBrf5rkmwFzsbWaGCnRMf59_TKZ9MS5dXXI438mFQ8h7ztaccfnxuMbjFKcBpxH8WjAhqr5pWfuCrLhWuulkq1-SFWOCNWojxWvyJucjq-yGqRX5_e0Kg020HCCNsYHB5oKe5mIdDlguNAY624TWDVBVDGGCnKk_pxmf0YAuQabOZujpYC-Q6vRxPMWMBagDO9bbC82Hxd1DiGm8xpWEP-IUR6gHf_XRMfYwVPh8GmrILyyHRcKA18ipLlDOBWeg8PNsC1blLXkV7JDh3fO8I98_f3raPTT7xy9fd_f7xgvdlabVwYECxp3qdBek3CoJgTNpewHaSe6E33jne5A6dFvldFBb55RjQapWtu0d-XDLPdjBnBKONl1MtGge7vdm0erHi05oMfPq3d68PsWcE4S_AGdmac4czT_NmaU5c2uusrsbC_UxM0Iy2SNMHnpM4IvpI_5Hyh9vVa9D</recordid><startdate>202301</startdate><enddate>202301</enddate><creator>Manickam, Ganapathi</creator><creator>Haboussi, Mohamed</creator><creator>D’Ottavio, Michele</creator><creator>Kulkarni, Vedang</creator><creator>Chettiar, Alfred</creator><creator>Gunasekaran, Vijay</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>AAYXX</scope><scope>CITATION</scope><scope>1XC</scope></search><sort><creationdate>202301</creationdate><title>Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations</title><author>Manickam, Ganapathi ; Haboussi, Mohamed ; D’Ottavio, Michele ; Kulkarni, Vedang ; Chettiar, Alfred ; Gunasekaran, Vijay</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c285t-38fbe7e01b7585f66976ef106ad2e8b61b2c4cbcde68f597b8f79bb7b0f673633</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Beam deflection</topic><topic>Curvilinear fibre angles</topic><topic>Engineering Sciences</topic><topic>Mechanics</topic><topic>Nonlinear thermo-elastic stability</topic><topic>Rotational spring</topic><topic>Structural mechanics</topic><topic>Thermal buckling</topic><topic>Thermal temperature rise</topic><topic>Variable stiffness composite beams</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Manickam, Ganapathi</creatorcontrib><creatorcontrib>Haboussi, Mohamed</creatorcontrib><creatorcontrib>D’Ottavio, Michele</creatorcontrib><creatorcontrib>Kulkarni, Vedang</creatorcontrib><creatorcontrib>Chettiar, Alfred</creatorcontrib><creatorcontrib>Gunasekaran, Vijay</creatorcontrib><collection>CrossRef</collection><collection>Hyper Article en Ligne (HAL)</collection><jtitle>International journal of non-linear mechanics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Manickam, Ganapathi</au><au>Haboussi, Mohamed</au><au>D’Ottavio, Michele</au><au>Kulkarni, Vedang</au><au>Chettiar, Alfred</au><au>Gunasekaran, Vijay</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations</atitle><jtitle>International journal of non-linear mechanics</jtitle><date>2023-01</date><risdate>2023</risdate><volume>148</volume><spage>104303</spage><pages>104303-</pages><artnum>104303</artnum><issn>0020-7462</issn><eissn>1878-5638</eissn><abstract>Nonlinear thermo-elastic buckling characteristics of composite variable stiffness beam with layers making use of curvilinear fibres under thermal environment is attempted here. The model is based on a shear deformable theory introducing trigonometric function, and considering von Kármán’s assumptions based geometrical nonlinear effect. The beam constitutive equation is modified according to the stress-free situation in the width direction of beam-Poisson’s effect in the formulation for predicting the behaviour of general lay-up composite beams. By the principle of minimum total potential energy, the governing equations in terms of incremental stiffness matrices are formed introducing general beam finite element. The global equilibrium equations formulated are solved for envisaging the post-buckling path through eigenvalue analysis iteratively, thus establishing the relationship of thermal temperature against moderate amplitude level of beam deflection. A systematic parametric analysis considering different lamina properties such as curvilinear fibre path angles and including lay-up sequences, thermal expansion coefficient, mixed laminate combining straight and curvilinear fibres-based layers is carried out on thermo-structural stability of curvilinear fibre-based beams. Also, the influence of geometric factors, flexible beam end support, and variation in thermal profile, etc. over the stability behaviour of beam is examined.
•Studied the nonlinear thermo-elastic stability of general lay-up composite beams using modified constitutive equations.•Established the nonlinear thermal elastic stability region of composite beams including the effects of curvilinear fibres.•Predicted the temperature rise after buckling against beam deflection, exhibiting varied hard spring type behaviour.•Confirmed the beam equilibrium state change associated with the instability in the nonlinear region.•Wide range of parametric analysis made here form benchmark solutions for other analytical/numerical models.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.ijnonlinmec.2022.104303</doi></addata></record> |
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subjects | Beam deflection Curvilinear fibre angles Engineering Sciences Mechanics Nonlinear thermo-elastic stability Rotational spring Structural mechanics Thermal buckling Thermal temperature rise Variable stiffness composite beams |
title | Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations |
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