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Master Thesis - OUFTI-1

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environment. Then, this model is exploded in several parts to isolate each component.<br />

Finally, a behavior and a material are assigned to each of them and they are linked together<br />

using the assembly methods available in Samcef (the methods used must be as close as<br />

possible from the real connection between the two components to obtain accurate results).<br />

5.2.1 Materials properties<br />

Firstly, the properties of the materials used for manufacturing the several components,<br />

are presented in a single table (see Table 5.1). This allows to avoid multiple repeatings of<br />

tables including these properties through this section. Afterwards, these materials will be<br />

just mentioned and their properties will not be reminded. It should be noted that these<br />

properties were found using the CES software.<br />

Materials Young's moduli (GP a) Poisson ratios Densities (kg/m 3 )<br />

Al − 5052 H32 71.795 0.33675 2685<br />

Al − 5754 69 0.33 2700<br />

Al − 7075 T 6 72.5 0.33 2800<br />

Al − 7075 T 73 71 0.33 2800<br />

FR 4 20 0.3 2200<br />

Stainless steel 205 0.3 7850<br />

Table 5.1: Properties of the materials used in <strong>OUFTI</strong>-1<br />

5.2.2 Main structure<br />

The main structure of <strong>OUFTI</strong>-1, which corresponds to the CSK structural parts,<br />

was modeled using shell components. Indeed, the thickness of the base and end plates<br />

(1.52 mm) and the one of the chassis (1.27 mm) are negligible with regard to their other<br />

dimensions (100 mm), which allows to use this type of modeling. All these components<br />

are made of Al − 5052 H32.<br />

The base and end plates are connected to the chassis by several M3 × 4 mm stainless<br />

steel screws. To model this type of connection in Samcef, the procedure is the following<br />

one:<br />

• A point (vertex) is placed at the center of the two holes (one on the considered plate<br />

and the other on the chassis).<br />

• These vertex are linked to the wire of their respecting hole using a "mean" assembly.<br />

This type of assembly determines the mean rotation and displacement of the nodes<br />

102

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