a fokker 70 aircraft is trimmed for steady level flight at a speed of 200 m s tas at an altitude of 10 000 m above sea level where the air density 0 41351 kg m 3 relevant characteristics of the aircraft are tabulated below

  1. B2(a) Calculate the lift coefficient of the aircraft.
  2. B2(b) Calculate the lift coefficient of the tailplane (Assume dynamic pressure is same at tail and wing)
  3. B2(c) Calculate the lift force produced by the tailplane.
  4. B2(d) Determine angle of attack of the tailplane with the tab undeflected.
  5. B2(e) Determine the elevator angle required to trim the aircraft with the tab undeflected.
  6. B2(f) Determine the stick position required to trim the aircraft with the tab undeflected.

(3 marks) (4 marks) (3 marks) (6 marks) (6 marks) (3 marks)

 
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