Elastoplastic Buckling of Functionally Graded Beams using Tamura-Tomota-Ozawa and Ramberg-Osgood Material Models
| dc.contributor.author | Sundaram Ezhilarasi, Ganesh Aravind | en |
| dc.contributor.committeechair | Kapania, Rakesh K. | en |
| dc.contributor.committeemember | Saha, Sourav | en |
| dc.contributor.committeemember | Wang, Kevin Guanyuan | en |
| dc.contributor.department | Aerospace and Ocean Engineering | en |
| dc.date.accessioned | 2026-06-17T08:02:14Z | en |
| dc.date.available | 2026-06-17T08:02:14Z | en |
| dc.date.issued | 2026-06-16 | en |
| dc.description.abstract | Functionally Graded Materials (FGMs) are an advanced class of composite materials characterized by a gradual, continuous variation of material properties spatially. While buckling of slender Functionally Graded Beams (FGBs) can be analyzed using linear eigenvalue analysis and is well documented, the buckling response of FGBs with low and medium slenderness ratios is under-researched. This behavior is highly complex due to coupled shear effects and material yielding in the elastoplastic region. The goal of this work is to investigate the nonlinear elastoplastic buckling of short and medium metal-ceramic FGBs. The beam kinematics are modeled using the First-Order Shear Deformation Theory (Timoshenko beam theory) within a semi-analytical Ritz framework. To simulate the elastoplastic behavior of FGBs, a modified rule-of-mixtures law, based on the Tamura-Tomota-Ozawa model, is coupled with the Ramberg-Osgood phenomenological constitutive equations. The nonlinear stress-strain behavior of the metal component of the FGB is described using Hencky's total plastic strain model. Finally, an arc-length solver is employed to trace the FGB's nonlinear load-displacement path. Parametric studies are conducted by varying power-law coefficients and thickness ratios, and the results are compared with those from a 3D Finite Element Analysis (FEA) using Abaqus/Standard. The analytical model demonstrates excellent agreement with FEA for beams with a medium length-to-thickness ratio, with a maximum error of just about 4% for thickness ratios > 15. However, some discrepancies are observed when comparing very short FGBs with thickness ratios between 5 and 15. These discrepancies stem from the fundamental divergence between the deformation theory of plasticity employed in this formulation and the flow theory used in FEA models, which highlights the 'plastic buckling paradox', and from differences between 3D FEA and 1D First-Order Shear Deformation Theory, reinforcing the critical need for experimental validation. | en |
| dc.description.abstractgeneral | As humanity pushes further into space with programs aiming for the Moon and Mars, engineers need materials that can survive extreme environments. Functionally Graded Materials (FGMs) are one such class of material. They are advanced composites that gradually blend two or more materials to leverage the best of both. Usually, these materials are tough ceramics with flexible metals. While engineers have a good understanding of how long, thin FGM beams fail under compressive loads (usually by bowing outward under pressure, called buckling), the failure of short, thick beams is relatively not well understood. In short beams, the material often permanently squishes (yield) under heavy loads before the beam can actually buckle. This thesis investigates exactly how and when these short metal-ceramic beams collapse. Instead of relying on simplified assumptions, a specialized computational model was developed to capture three complex factors simultaneously: the beam's physical bending, the metal component's permanent yielding, and the intricate interactions between these mixed materials. When tracking beam deformation under compressive loads, the new model proved highly accurate for long and medium-length beams, matching industry-standard software with a maximum error of just 4%. However, for the very shortest beams, the model revealed significant differences, highlighting a famous structural engineering phenomenon known as the "plastic buckling paradox". Ultimately, this work aims to provide an efficient tool for aerospace designers while proving that physical, real-world testing is absolutely critical to guarantee the safety of short FGM beams. | en |
| dc.description.degree | Master of Science | en |
| dc.format.medium | ETD | en |
| dc.identifier.other | vt_gsexam:47072 | en |
| dc.identifier.uri | https://hdl.handle.net/10919/143446 | en |
| dc.language.iso | en | en |
| dc.publisher | Virginia Tech | en |
| dc.rights | In Copyright | en |
| dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
| dc.subject | Functionally graded beams | en |
| dc.subject | Elastoplastic analysis | en |
| dc.subject | Buckling | en |
| dc.subject | Ritz method | en |
| dc.subject | Arc-length solver | en |
| dc.title | Elastoplastic Buckling of Functionally Graded Beams using Tamura-Tomota-Ozawa and Ramberg-Osgood Material Models | en |
| dc.type | Thesis | en |
| thesis.degree.discipline | Aerospace Engineering | en |
| thesis.degree.grantor | Virginia Polytechnic Institute and State University | en |
| thesis.degree.level | masters | en |
| thesis.degree.name | Master of Science | en |
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