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Given that s - 20o ft*; C6 ft.; symmetrical untwisted wing. s^-- 40 ft2; tail aero. centre is 22 ft aft of wing L.E. t 0.44b = (SCL/aO)0.08 per deg. (SC^/a0.07 per deg. 0.05 per deg. Assume aero. centre of wing is at 0.25 mean aerodynamic chord and that Cac a) Find the location of the stick-fixed neutral point for this aircraft. b) If the weight of the aircraft of problem 2 is 3000 1b. and if its centre of gravity is at 0.333 mean aerodynamic chord, find the dynamic pressure 1/2 2 (do not neglect tail lift) required for trim with zero elevator angle. 22 Ibe/ft2, find the ) If the aircraft speed is such that 1/20^v 2 - elevator angle for trim, if aircraft weight and C.G. position are the same as in b) Given that s - 20o ft*; C6 ft.; symmetrical untwisted wing. s^-- 40 ft2; tail aero. centre is 22 ft aft of wing L.E. t 0.44b = (SCL/aO)0.08 per deg. (SC^/a0.07 per deg. 0.05 per deg. Assume aero. centre of wing is at 0.25 mean aerodynamic chord and that Cac a) Find the location of the stick-fixed neutral point for this aircraft. b) If the weight of the aircraft of problem 2 is 3000 1b. and if its centre of gravity is at 0.333 mean aerodynamic chord, find the dynamic pressure 1/2 2 (do not neglect tail lift) required for trim with zero elevator angle. 22 Ibe/ft2, find the ) If the aircraft speed is such that 1/20^v 2 - elevator angle for trim, if aircraft weight and C.G. position are the same as in b)