Calculate the coefficient of lift and coefficient of drag for the body shown below. Neglect the rear surface of the body. The chord of this body is taken to be the lower surface with a length of 1.5 meters. Angle of attack is +10 degrees. (Not drawn to scale). Pu,1 = 100 kpa, Tu = 200 * S-0.3 pa 1 m Pi = (140 60 S)kpa , t = 200 S-0.3 pa 10 degrees