For the data shown in Fig. P2.2, determine the following. (a) The stick fixed neutral point. (b) If we wish to fly the airplane at a velocity of 125 ft/s at sea level, what would be the trim lift coefficient and what would be the elevator angle for trim? w- 2,750 lb S- 180 ft 2 cg - 0.25 7 0.15 0.10 0.05 - CL 0.0 0.6 0.8 1.0 0.2 0.4 de --15 -0.05 - -10 -0.10 -5 0 be -0.15 5 de FIGURE P2.2