Dry Fabric Forming Analysis Considering the Influence of Tensions on In-plane Shear Behavior

Abstract

In this study, we propose a FE model for dry fabric forming simulation that can express the tension dependent shear behavior in order to predict the wrinkles, one of the major forming defects. Automakers are gradually using more carbon fiber reinforced plastic (CFRP) in mass production cars, because the development of resin transfer molding (RTM) have reduced its cycle time to less than 10 minutes. Finite element analysis (FEA) is essential to the vehicle design process, so numerical simulation of CFRP is strongly desired today. Forming simulation is especially important, because the performance of the final composite part strongly depends on changes in fiber orientation during the preforming. Moreover wrinkle is one of the major defects in preforming. RTM usually involves fabric reinforcement. During forming of fabric, large in-plane shear deformations typically occur. The reason for this is that the shear resistance is very low at the initial stage, because the deformation is governed by yarn contact friction at the cross-sections. Accurately expressing the in-plane shear behavior of fabric is very important for accurate forming simulation. In most simulation models the shear resistance of fabric is assumed to be independent from the tension along the yarn. However, meso-model predictions of the picture frame and bias-extension tests suggest this to be an invalid assumption. In this study, a micromechanical model that introduces the stress component due to the yarn rotational friction is adapted to the dry fabric forming simulation. In other words, this can express the shear behavior that depends on the tensions in the yarns. The results using this micromechanical model are in good agreement with the meso-model results in the various boundary conditions. ．その † 原稿受理 平成25年9月10日 Received

Analysis and Modeling of Wrinkling in Composite Forming

“…Using finite shell elements and remaining within the framework of classical shell theory, some approaches modify the ratio between bending and tension stiffnesses. The textile reinforcement can be seen as a laminate composed of layers of different Young's modulus so that both tensile and bending stiffnesses are achieved (Figure 5b,c) [64,65]. The superposition of a membrane finite element and a pure bending shell element is also a way to decouple the two behaviors.…”

“…Figure 5. Introduction of bending stiffness into a textile fabric: (a) combination of beam and membrane elements [62],(b,c) fibrous fabric considered as a laminate[64,65].…”

Contributions of Stepan V Lomov to the research and development of composite materials

“…61 The macroscopic simulations concern the entire textile reinforcement and use shell finite elements specific to textiles. 62 Based on their results, risk areas are analysed on a mesoscopic scale. Each yarn is modelled by 3 D finite elements and a hyperelastic behaviour law specific to fibrous yarns.…”

Modeling and analysis of in-plane bending in fibrous reinforcements with rotation-free shell finite elements.

“…DKT) (Haanappel et al, 2014;Dörr et al, 2018) or membrane and beam elements (Harrison et al, 2013;Dangora et al, 2015;Mitchell et al, 2016;Giorgio et al, 2018). Modifications of the properties in the thickness were also proposed in order to obtain the desired membrane stiffness and bending (Yu et al, 2005b;Gereke et al, 2013;Nishii et al, 2014;Dangora et al, 2015). A shell approach specific to fibrous reinforcements has also been proposed (Liang et al, 2017).…”