2. Let's do the airplane wing example we saw on video in class... Assume we have the wing of a large airliner. The wing can be approximated by considering it as a long rectangle that is 50 feet long, by 10 feet wide by 6 inches in height. Let's also assume the wing is made of aluminum and that there is a 20,000 lb-load applied in the upward direction at the end of the wing. We will neglect the weight of the wing itself. Using the 4th order load deflection equation determine: a. The deflection of the wing at 50% of the wing length; b. The slope of the wing at the full length of the wing. Given: 4th order LD Equation: (El(v(x)")" = P(x) Ealuminum = 10.6 x 106 psi Rectangle = bh3/12 Boundary Values: = V(O) = -20,000 lbf M(50 feet) = 0 V (0) = 0 V(O) = 0 HINT: Watch your units and make sure you show 4 integrations and solutions for C...C