An Airbus A300 aircraft is flying at h = 10000m (air density p=0.4127kg/m) in a steady level turning flight at 80% throttle setting with a bank angle u = 30. The A300 has the following properties in the usual notation: S = 260m? b = 44.8m CLO = 0.141 Tmax = 452KN CLa = 0.11 CME = -0.013 CDo = 0.023 CLmax = 2.7 CMO = -0.0092 m=130000kg meng = 0.6 k = 0.059 nmax = 2.5 CMa = -0.018 %3D %3D (a) Determine the airspeeds for all possible flight conditions for this coordinated turn. (b) Determine the turn radius and turn rate for all possible flight conditions for this coordinated turn. (c) Determine the angle of attack and elevator deflection angle for all possible flight conditions for this coordinated turn.