Melbourne Institute of Technology Fokker 70 Aircraft Lift Coefficient Paper
- B2(a) Calculate the lift coefficient of the aircraft.
- B2(b) Calculate the lift coefficient of the tailplane (Assume dynamic pressure is same at tail and wing)
- B2(c) Calculate the lift force produced by the tailplane.
- B2(d) Determine angle of attack of the tailplane with the tab undeflected.
- B2(e) Determine the elevator angle required to trim the aircraft with the tab undeflected.
- B2(f) Determine the stick position required to trim the aircraft with the tab undeflected.
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