Abstract
AbstractThe benefits of incorporating rubber interlayers in lightweight laminates, such as fiber‐metal laminates, in order to compensate for their usually undesirable dynamic behavior have been studied in previous works [1,2]. In such constrained‐layer damping laminates, the rubber layers undergo large deformations due to their comparably low stiffness. This motivates the consideration of large strain phenomena commonly found in rubbers even when global laminate deformations are small such as in linear dynamic analysis. This work specifically addresses the cyclic softening of filled rubbers commonly known as the Mullins effect. As this effect significantly influences the elastic properties of the material, a change in the dynamic behavior of the laminate is to be expected. A constitutive model based on the work of Dorfmann and Ogden [3] for the prediction of the cyclic softening as well as residual strains upon unloading is presented in this study. Special consideration is given to the implementation of the model for use in a commercial implicit finite element solver by building on the work of Connolly et al. [4]. The model is validated against experimental data and compared to a current state‐of‐the‐art model with regard to its predictive quality and computational efficiency. Furthermore, the experimental identification of material parameters for said model is addressed.
Highlights
Lightweight structures by nature feature comparably high stiffness with a low mass
The Mullins effect is a large strain phenomenon, it should be considered in the modeling of constrained-layer damping (CLD) applications, as the strains observed in the damping layers exceed the global deformation of the laminate by far
This work deals with the experimental characterization and constitutive modeling of a rubber material used in CLD applications
Summary
Lightweight structures by nature feature comparably high stiffness with a low mass. This can lead to vibration and undesirable dynamic behavior. Filled rubbers are used as damping layers in CLD applications. The Mullins effect is a large strain phenomenon, it should be considered in the modeling of CLD applications, as the strains observed in the damping layers exceed the global deformation of the laminate by far. Deformations during manufacturing or assembly and possible static loads during operation can trigger the Mullins effect and affect the mechanical behavior of the damping layer. This work deals with the experimental characterization and constitutive modeling of a rubber material used in CLD applications. The chosen pseudo-elastic model is formulated in principal stretches in order to be used in a commercial Finite Element Method (FEM) code
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