Abstract
Unidirectional non-crimp fabrics (UD-NCF) are often used to exploit the lightweight potential of continuous fiber reinforced plastics (CoFRP). During the draping process, the UD-NCF fabric can undergo large deformations that alter the local fiber orientation, the local fiber volume content (FVC) and create local fiber waviness. Especially the FVC is affected and has a large impact on the mechanical properties. This impact, resulting from different deformation modes during draping, is in general not considered in composite design processes. To analyze the impact of different draping effects on the mechanical properties and the failure behavior of UD-NCF composites, experimental results of reference laminates are compared to the results of laminates with specifically induced draping effects, such as non-constant FVC and fiber waviness. Furthermore, an analytical model to predict the failure strengths of UD laminates with in-plane waviness is introduced. The resulting stiffness and strength values for different FVC or amplitude to wavelength configurations are presented and discussed. In addition, failure envelopes based on the PUCK failure criterion for each draping effect are derived, which show a clear specific impact on the mechanical properties. The findings suggest that each draping effect leads to a “new fabric” type. Additionally, analytical models are introduced and the experimental results are compared to the predictions. Results indicate that the models provide reliable predictions for each draping effect. Recommendations regarding necessary tests to consider each draping effect are presented. As a further prospect the resulting stiffness and strength values for each draping effect can be used for a more accurate prediction of the structural performance of CoFRP parts.
Highlights
One of the main challenges in the design of structural components using fiber reinforced plastics is the impact of the manufacturing process on the resulting structural performance [1,2]
The resulting material properties for reference samples at the three different fiber volume content (FVC) of 48 %, 54 % and 60 % are summarized in Tables 8 and 9 with median values and the corresponding interquartile range
Since the increase of E1 depends on the carbon fiber itself, the slope dE1/dε 11 should increase with increasing FVC
Summary
One of the main challenges in the design of structural components using fiber reinforced plastics is the impact of the manufacturing process on the resulting structural performance [1,2]. While forming simulations on a macroscopic level provides reliable results regarding the local fabric deformations [4], the actual material properties of the composite are defined after the infiltration step as soon as the laminate is fully cured. It is possible to manipulate the fabric deformation by specific manufacturing process boundary conditions [6,7,8], a homogeneous distribution of the FVC, without any local gapping or fiber waviness, is difficult to achieve. One of the commonly used fabric types for the production of CoFRP parts are unidirectional non-crimp fabrics (UD-NCF) due to their straight fibers without inherent undulations. This fabric type typically undergoes several deformation modes (cf Figure 1)
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