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SAWE Report - Cal Poly San Luis Obispo

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The layout of Vendetta’s inlets and landing gear allow for a continuous structural member, in the<br />

form of a bulkhead, to carry the aerodynamic loads from each wing directly to the central keel.<br />

This ideology breaks down as the bulkheads move away from the main wing load paths. The<br />

weapons bay splits the forward wing attachment bulkheads. This occurs only well in front of the<br />

aerodynamic center of the wing. Just forward of the aerodynamic center is the main forward<br />

load path for the wing. The aft load paths are a ring structure around the engines and inlets. The<br />

Important thing to note is that where the primary loads are being distributed, between 25 to 50<br />

percent of the mean aerodynamic chord, the bulkheads are continuous.<br />

It is also important to note that the landing gear attaches to a bulkhead just forward of the aft<br />

closure to the weapons bay. This is important because it locates the airborne and ground laden<br />

load paths on top of each other. This allows for some redundancy in the structure and allows for<br />

a lighter aircraft. Another redundant feature is the aft main load path. This bulkhead acts as the<br />

main forward engine attachment point. Again this allows for a minimum of large structural<br />

bulkheads and thus creates a lighter aircraft. The wing attachment points are shown in Figure<br />

7.2.<br />

The empennage structure follows the same methodology as the wing attachment structure. The<br />

vertical tails attach to the aft primary carry through of the wing. The aft vertical attach point is<br />

the same as the primary load path for the horizontal tails. The horizontal tail is an area of<br />

concern for the Vendetta. The horizontal surfaces are capable of producing tremendous forces on<br />

the aircraft. The horizontal surfaces are full flying and thus must attach at a single point in the<br />

aircrafts structure. This bulkhead is a ring carry through type that distributes the load from the<br />

pivot point to the central keel. Two secondary bulkheads back up this main bulkhead. The<br />

empennage structure is shown in Figure 7.3.<br />

Aft Primary<br />

Bulkhead & Main<br />

Engine Attachment<br />

Forward Secondary<br />

Bulkheads<br />

Forward Primary<br />

Bulkhead<br />

Aft Secondary<br />

Bulkheads<br />

Main Gear<br />

Attachment<br />

Figure 7.2 - Wing Attachment Detail<br />

49

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