Final Design Report - Purdue University
Figure 6 1: Simple Cantilever Beam (Wing) Using the representation shown in Figure 6 1, a formula for the deflection at the tip of the spar can be seen in Equation 6 1. In this equation, E is the Young’s Modulus of the material, and I is the moment of inertia of the spar. This equation was plotted for a variety of different spar sizes. ................
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