Investigations on the linear vibration characteristics of bistable unsymmetrical laminates
| dc.contributor.author | Anilkumar P.M.; Rao B.N.; Haldar A.; Scheffler S.; Wolniak M.; Rolfes R.; Jansen E.L. | |
| dc.date.accessioned | 2025-05-23T11:24:31Z | |
| dc.description.abstract | Linear vibration characteristics of bistable unsymmetric laminates have been explored in this study. An experimental strategy to capture the natural frequencies of a bistable composite laminate is presented. An unsymmetric cross-ply laminate supported at its centre and free at all boundaries has been used for the experimental testing. The present study considers the small-amplitude natural vibrations around the static equilibrium shapes where the vibrations are measured using miniature integrated electronics piezoelectric (IEPE) accelerometer sensors. An improved semi-analytical framework where Hamilton’s principle is applied in combination with the Rayleigh-Ritz approach is proposed to analyse the vibration characteristics of the selected bistable laminate. In this framework, the membrane and bending energies are decoupled by a semi-inverse constitutive equation. The in-plane stress components are expressed as differential equations in terms of curvatures using the in-plane equilibrium equations and the compatibility conditions, and the obtained equations are converted into the form of a standard finite element elasticity problem. The in-plane stress components are separately evaluated by solving the obtained finite element elasticity problem using a standard numerical approach. As a result, the total potential energy is expressed in terms of the unknown coefficients of the assumed out-of-plane displacement function. In the subsequent dynamic analysis, perturbations are imposed on the static equilibrium configurations to simulate the eigenfrequencies and corresponding eigenmodes. The proposed semi-analytical model is computationally efficient and very effective to predict the linear vibration characteristics of bistable unsymmetric laminates. The solutions are further compared with a fully geometrically nonlinear FE calculation. © 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. | |
| dc.identifier.doi | https://doi.org/10.2514/6.2022-0258 | |
| dc.identifier.uri | http://172.23.0.11:4000/handle/123456789/10163 | |
| dc.relation.ispartofseries | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 | |
| dc.title | Investigations on the linear vibration characteristics of bistable unsymmetrical laminates |