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PFR - Aerospace Engineering Sciences Senior Design Projects ...

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Project Final Report – CUDBF April 30 th , 2009<br />

ASEN 4028: <strong>Aerospace</strong> <strong>Senior</strong> <strong>Projects</strong><br />

11.2 Wing Sub-Assembly<br />

The wing sub-assembly consists of the main wing assembly and the vertical assembly.<br />

11.2.1 Wing Assembly<br />

The main wing assembly is composed of a core of 1pcf EPS foam. The foam cores will be<br />

outsourced due to the geometric twist of the wing. This will ensure that the foam cores are the<br />

correct dimensions. The balsa motor mount blocks are then glued into the foam using epoxy.<br />

Also, the main gear mount plywood mount will be glued into the core before sheeting. The foam<br />

core will then skinned with 1/32” light weight balsa. The control surfaces will also be sheeted<br />

with 1/32” light weight balsa after a balsa insert is glued into the foam for the control horn. The<br />

ailerons and elevators will then be attached to the wing halves. Both wing halves will be<br />

constructed in parallel and can be seen below in Figure 95.<br />

Figure 95: Main Wing Assembly<br />

11.2.2 Vertical Tail Assembly<br />

The foam cores for the verticals will also be outsourced in order to achieve the desired<br />

tolerances. The verticals and rudders will be sheeted the same way as previously mentioned.<br />

After they are sheeted, the carbon support tubes will be inserted and glued in place. These will<br />

then be glued to the balsa vertical spar mount. The rudders will then be attached to each winglet.<br />

Both vertical tails will be constructed in parallel. A vertical tail can be seen in Figure 96.<br />

116

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