The wing of the glider shown above has an aspect ratio of 15, and its airfoil is an NACA 63-210. The span efficiency is 90% and the wing area is 224f^2. The wing is flying at 3 degrees angle of attack. The glider is crusing at 80 knots at 10,000 feet. Assume the Reynolds number is 9(10)^6. Determine the three-dimensional lift and drag coefficients, and the lift and drag for the wing. Solve the problem in the English system of units.