Validation of the numerical model of single-layer composites reinforced with carbon fiber and aramid
In this work we studied the experimental validation of the model and finite element analysis for a single layer of composite materials reinforced with carbon (denoted as C), aramid (K) and carbon-aramid (C-K) fibers. In the literature there are not many details about the differences that arise betwe...
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Sprache: | eng |
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Zusammenfassung: | In this work we studied the experimental validation of the model and finite element analysis for a single layer of composite materials reinforced with carbon (denoted as C), aramid (K) and carbon-aramid (C-K) fibers. In the literature there are not many details about the differences that arise between transversal and longitudinal characteristics of composite materials reinforced with fabric, compared to those with unidirectional fibers. In order to achieve carbon and aramid composites we used twill fabric and for carbon-aramid plain fabric, as shown in Figure 1.
In order to observe the static behavior of the considered specimens, numerical simulations were carried out in addition to the experimental determination of the characteristics of these materials.
Layered composites are obviously the most widespread formula for getting advanced composite structures. It allows a unique variety of material and structural combinations leading to optimal design in a wide range of applications [1,2].
To design and verify the material composites it is necessary to know the basic mechanical constants of the materials. Almost all the layered composites consider that the every layer is an orthotropic material, so there are nine independent constants of material corresponding to the three principal directions: Young modulus E
1, E
2 and E
3, shear modulus G
12, G
23 and G
13, and major poison ratios ν12, ν23, ν13.
Experimental determinations were performed using traction tests and strain gauges. For each of the three above mentioned materials, five samples were manufactured. |
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ISSN: | 0094-243X 1551-7616 |
DOI: | 10.1063/1.4952316 |