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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Rolfes, Raimund
Leibniz University Hannover
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (20/20 displayed)
- 2024Evaluating the mechanical behavior of carbon composites with varied ply-thicknesses using acoustic emission measurements
- 2024A thermodynamically consistent physics-informed deep learning material model for short fiber/polymer nanocompositescitations
- 2024Phase-field modeling of fracture in viscoelastic–viscoplastic thermoset nanocomposites under cyclic and monolithic loading
- 2023Analysis of fatigue crack and delamination growth in GFRP composites in tension and compression loading
- 2023Refined Semi-Analytical Framework to Predict the Natural Vibration Characteristics of Bistable Laminatescitations
- 2023A new base of wind turbine noise measurement data and its application for a systematic validation of sound propagation modelscitations
- 2022Effect of moisture on the nonlinear viscoelastic fracture behavior of polymer nanocompsites: a finite deformation phase-field model
- 2022Efficient generation of geodesic random fields in finite elements with application to shell bucklingcitations
- 2021Robust improvement of the asymmetric post-buckling behavior of a composite panel by perturbing fiber paths
- 2020An efficient semi-analytical framework to tailor snap-through loads in bistable variable stiffness laminatescitations
- 2019Evaluation and modeling of the fatigue damage behavior of polymer composites at reversed cyclic loadingcitations
- 2019Progressive Failure Analysis Using Global-Local Coupling Including Intralaminar Failure and Debondingcitations
- 2018Effect of spatially varying material properties on the post-buckling behaviour of composite panels utilising geodesic stochastic fields
- 2018Effect of spatially varying material properties on the post-buckling behaviour of composite panels utilising geodesic stochastic fields
- 2018Experimental characterization and constitutive modeling of the non-linear stress–strain behavior of unidirectional carbon–epoxy under high strain rate loadingcitations
- 2018Analysis of skin-stringer debonding in composite panels through a two-way global-local methodcitations
- 2018A structural design concept for a multi-shell blended wing body with laminar flow control
- 2015An elastic molecular model for rubber inelasticitycitations
- 2014Material Modelling of Short Fiber Reinforced Thermoplastic for the FEA of a Clinching Test
- 2014Investigating the VHCF of composite materials using new testing methods and a new fatigue damage model
Places of action
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article
Refined Semi-Analytical Framework to Predict the Natural Vibration Characteristics of Bistable Laminates
Abstract
<jats:p> Bistable unsymmetrical laminates have received significant attention in morphing applications due to their ability to attain multiple shapes when subjected to thermal loads. Morphing structures in general are subjected to dynamic operating conditions. Also, the highly nonlinear snap-through transition between stable configurations possesses rich dynamic characteristics. Therefore, understanding the dynamic characteristics of bistable laminates is essential for designing morphing structures constituting bistable elements. Thus, the present study aims to explore the dynamics of bistable unsymmetrical laminates by evaluating their natural vibration characteristics associated with small-amplitude dynamic excitation around the static equilibrium configurations. A refined semi-analytical framework is proposed to analyze the natural vibration characteristics of the bistable laminate, where the potential energy is expressed only in terms of the unknown coefficients of the assumed out-of-plane displacement function. The in-plane components are separately evaluated using the in-plane equilibrium equations and compatibility conditions. In the dynamic analysis, perturbations are imposed on the static equilibrium configurations to capture the modal characteristics. A full geometrically nonlinear finite element (FE) model of the bistable laminate has been created in a commercially available FE package to compare semi-analytical solutions. To validate the proposed frameworks, an experimental strategy to capture the natural frequencies of a bistable laminate is presented in this paper. Unsymmetric laminates mounted at its center have been used for the experimental testing, where the vibrations are measured using miniature integrated electronics piezoelectric accelerometer sensors attached at the corners. The semi-analytical and FE results are validated against the experimental observations for the selected unsymmetrical cross-ply laminates. The proposed frameworks are further extended to a family of unsymmetrical variable-stiffness (VS) laminates generated using curvilinear fiber alignments. The selected VS family can generate bistable shapes without any twisting curvature similar to that of an unsymmetrical cross-ply laminate, where the designer can expand the design space with a plethora of multiple configurations. A parametric study is performed by tailoring the VS parameters to investigate the influence of curvilinear fiber alignments on the natural vibration characteristics of bistable VS laminates. </jats:p>