Non-linear thermal stability and free vibration behavior of sandwich beams with auxetic re-entrant aluminum cores and graphene origami-enhanced facings

dc.contributor.authorShashiraj
dc.contributor.authorPitchaimani, J.
dc.contributor.authorKattimani, S.
dc.date.accessioned2026-02-03T13:19:10Z
dc.date.issued2025
dc.description.abstractRevolutionizing advanced sandwich structures, this study delves into the non-linear thermal stability behavior and free vibration characteristics of auxetic aluminum re-entrant core sandwich beams enhanced with graphene origami (GOri) metamaterial facings, subjected to spatially varying thermal environment. The sandwich beams are modeled as layered structures incorporating complex geometric non-linearities, using a higher-order shear deformation framework and non-linear strain–displacement kinematics based on von Kármán assumptions. The governing equations of motion are addressed through the Ritz formulation, enabling an in-depth investigation of how variations in graphene origami layout, concentration, and fold geometry within the face sheets influence the structural performance. Additionally, the influence of various core Poisson's ratio configurations-negative (NPR), zero (ZPR), and positive (PPR)-along with the effects of core angle and thickness ratio, are systematically explored. The results highlight that core topology critically influences post-buckling resistance and non-linear vibrational characteristics. Furthermore, the integration of graphene origami significantly enhances stiffness and structural stability, demonstrating its potential for next-generation aerospace, automotive, and high-performance engineering applications. To the best of the authors’ knowledge, this is the first study to explore the coupled effects of auxetic re-entrant aluminum cores and graphene origami-enhanced facings on the non-linear thermal and dynamic behavior of sandwich beams. © 2025 Elsevier Ltd
dc.identifier.citationComposite Structures, 2025, 372, , pp. -
dc.identifier.issn2638223
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2025.119564
dc.identifier.urihttps://idr.nitk.ac.in/handle/123456789/19987
dc.publisherElsevier Ltd
dc.subjectAluminum
dc.subjectBuckling
dc.subjectBuckling behavior
dc.subjectFacings
dc.subjectMetamaterials
dc.subjectPoisson ratio
dc.subjectSandwich structures
dc.subjectShear flow
dc.subjectStructural analysis
dc.subjectThermodynamic stability
dc.subjectVibration analysis
dc.subjectAuxetic metamaterial
dc.subjectAuxetics
dc.subjectGraphene origami
dc.subjectGraphenes
dc.subjectLinear vibration analysis
dc.subjectNegative Poisson ratio
dc.subjectNon-linear vibrations
dc.subjectRe-entrant auxetic core sandwich beam
dc.subjectRitz methods
dc.subjectSandwich beams
dc.subjectThermal post-buckling
dc.subjectThermal post-buckling and non-linear vibration analyze
dc.subjectEquations of motion
dc.titleNon-linear thermal stability and free vibration behavior of sandwich beams with auxetic re-entrant aluminum cores and graphene origami-enhanced facings

Files

Collections