Non-linear thermal stability and free vibration behavior of sandwich beams with auxetic re-entrant aluminum cores and graphene origami-enhanced facings
| dc.contributor.author | Shashiraj | |
| dc.contributor.author | Pitchaimani, J. | |
| dc.contributor.author | Kattimani, S. | |
| dc.date.accessioned | 2026-02-03T13:19:10Z | |
| dc.date.issued | 2025 | |
| dc.description.abstract | Revolutionizing 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.citation | Composite Structures, 2025, 372, , pp. - | |
| dc.identifier.issn | 2638223 | |
| dc.identifier.uri | https://doi.org/10.1016/j.compstruct.2025.119564 | |
| dc.identifier.uri | https://idr.nitk.ac.in/handle/123456789/19987 | |
| dc.publisher | Elsevier Ltd | |
| dc.subject | Aluminum | |
| dc.subject | Buckling | |
| dc.subject | Buckling behavior | |
| dc.subject | Facings | |
| dc.subject | Metamaterials | |
| dc.subject | Poisson ratio | |
| dc.subject | Sandwich structures | |
| dc.subject | Shear flow | |
| dc.subject | Structural analysis | |
| dc.subject | Thermodynamic stability | |
| dc.subject | Vibration analysis | |
| dc.subject | Auxetic metamaterial | |
| dc.subject | Auxetics | |
| dc.subject | Graphene origami | |
| dc.subject | Graphenes | |
| dc.subject | Linear vibration analysis | |
| dc.subject | Negative Poisson ratio | |
| dc.subject | Non-linear vibrations | |
| dc.subject | Re-entrant auxetic core sandwich beam | |
| dc.subject | Ritz methods | |
| dc.subject | Sandwich beams | |
| dc.subject | Thermal post-buckling | |
| dc.subject | Thermal post-buckling and non-linear vibration analyze | |
| dc.subject | Equations of motion | |
| dc.title | Non-linear thermal stability and free vibration behavior of sandwich beams with auxetic re-entrant aluminum cores and graphene origami-enhanced facings |
