Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations

dc.contributor.authorManickam, G.
dc.contributor.authorHaboussi, M.
dc.contributor.authorD'Ottavio, M.
dc.contributor.authorKulkarni, V.
dc.contributor.authorChettiar, A.
dc.contributor.authorGunasekaran, V.
dc.date.accessioned2026-02-04T12:27:17Z
dc.date.issued2023
dc.description.abstractNonlinear 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. © 2022
dc.identifier.citationInternational Journal of Non-Linear Mechanics, 2023, 148, , pp. -
dc.identifier.issn207462
dc.identifier.urihttps://doi.org/10.1016/j.ijnonlinmec.2022.104303
dc.identifier.urihttps://idr.nitk.ac.in/handle/123456789/22196
dc.publisherElsevier Ltd
dc.subjectBuckling
dc.subjectComposite beams and girders
dc.subjectEigenvalues and eigenfunctions
dc.subjectFibers
dc.subjectFlexible structures
dc.subjectNonlinear equations
dc.subjectPoisson equation
dc.subjectPotential energy
dc.subjectShear deformation
dc.subjectShear flow
dc.subjectStability
dc.subjectStiffness
dc.subjectStiffness matrix
dc.subjectThermal expansion
dc.subjectThermoelasticity
dc.subjectBeam deflection
dc.subjectComposite beam
dc.subjectCurvilinear fiber angle
dc.subjectCurvilinear fibers
dc.subjectElastic stability
dc.subjectFiber angles
dc.subjectNonlinear thermo-elastic stability
dc.subjectRotational spring
dc.subjectTemperature rise
dc.subjectThermal
dc.subjectThermal buckling
dc.subjectThermal temperature rise
dc.subjectVariable stiffness
dc.subjectVariable stiffness composite beam
dc.subjectConstitutive equations
dc.titleNonlinear 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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