Bistable variable stiffness laminates - novel manufacturing and modeling strategies
Bistable laminates offer a path to energy-efficient and multi-functional structures, with potential applications in various engineering domains. Recent advancements in composites research indicate that replacing conventional straight fiber composites with Variable Stiffness (VS) composites opens up new avenues for enhancing the design space of shape-morphing structures. The production of VS laminates requires the use of advanced manufacturing techniques that enable the precise placement of composite tape modules in the specified orientations. This paper proposes an innovative approach to manufacturing bistable VS laminates, in which a detailed experimental campaign to manufacture and test bistable VS laminates is presented. Two specific sets of VS families have been selected, and their bistable shapes and snap-through requirements are systematically evaluated. The paper further seeks to provide validation for an efficient semi-analytical and numerical model proposed by the authors in their previous work by experimentally observing bistable characteristics. The theoretical and numerical predictions on generating a plethora of bistable configurations and tailoring the snap-through requirements using VS laminates are found to be in good agreement with experiments. The studies strengthen the conclusion that replacing conventional fibers with curvilinear fibers can substantially expand the design space, providing a diverse range of bistable shapes for morphing applications. • A novel manufacturing technique has been proposed to generate bistable variable stiffness laminates. • Existing semi-analytical and finite element frameworks are verified with experimental observations for bistable variable stiffness laminates. • Tailoring the bistable characteristics using variable stiffness laminates has been demonstrated through experiments. • The proposed novel manufacturing technique reduces the likelihood of conventional issues, such as gaps and overlaps during the production of bistable variable stiffness laminates.
Authors
- S. Scheffler (ORCID: https://orcid.org/0000-0002-9839-1753)
- Paul M. Weaver (ORCID: https://orcid.org/0000-0002-1905-4477)
- Gearóid J. Clancy
- P. M. Anilkumar (ORCID: https://orcid.org/0000-0001-5649-3260)
- B. N. Rao (ORCID: https://orcid.org/0000-0003-2988-3380)
- A. Haldar (ORCID: https://orcid.org/0000-0001-5448-9292)
- Raimund Rolfes (ORCID: https://orcid.org/0000-0001-7714-3382)
Institutions
- Leibniz University Hannover (DE)
- University of Limerick (IE)
- Indian Institute of Technology Madras (IN)
- University of Bristol (GB)
- Indian Institute of Technology BHU (IN)
- Banaras Hindu University (IN)
Publication Details
- Journal
- Materials & Design
- Published
- 2025-05-28
- DOI
- https://doi.org/10.1016/j.matdes.2025.114131
- Citations
- 4
- Primary Topic
- Aeroelasticity and Vibration Control
- Type
- article
- Field-Weighted Citation Impact
- 19.97
Funders
- Science Foundation Ireland
- Deutsche Forschungsgemeinschaft
- Gottfried Wilhelm Leibniz Universität Hannover
- Horizon 2020 Framework Programme
- H2020 Marie Skłodowska-Curie Actions