4.6 Article

Modeling bending behavior of shape memory alloy wire-reinforced composites: Semi-analytical model and finite element analysis

Journal

CHINESE JOURNAL OF AERONAUTICS
Volume 34, Issue 8, Pages 176-191

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2021.01.004

Keywords

Bending; Finite element analysis; Modelling; Phase transformation; Superelasticity; Shape memory alloy reinforced composite

Funding

  1. Khalifa University [CIRA 2019-024]

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A novel and simple exact semi-analytical model for superelastic SMA wire reinforced composites under bending loads is proposed in this study. The mechanical response of the composite is investigated using analytical equations and numerical simulations, showing that the composite exhibits superelastic behavior under certain conditions, which is beneficial for applications requiring large recoverable strains or high energy dissipation density.
In this study, we propose a novel and simple exact semi-analytical model for superelastic Shape Memory Alloy (SMA) wire reinforced composites subjected to bending loads. In order to study the mechanical response of the composite during loading/unloading, a Representative Volume Element (RVE) is extracted to examine the bending response of the composite. Analytical moment-curvature, and shear force-shear strain relations are derived based on a 3-Dimensional (3D) thermomechanical SMA model and Timoshenko beam theory. The composite Simpson's rule is adopted to numerically solve the exact analytical moment-curvature and shear force-shear strain relationships. Results including the moment-curvature response, axial stress distribution along the vertical and longitudinal directions, martensite volume fraction, and the tip deflection are reported and validated against 3D finite element simulations. The influence of temperature, martensite volume fraction distribution, and matrix stiffness on the mechanical performance of the composite is also investigated. In particular, the composite is found to behave superelastically under certain conditions of temperature, SMA volume fraction, and elastic stiffness of the matrix. Such behavior is advantageous in applications requiring large recoverable strains or high energy dissipation density. (c) 2021 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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