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Recap: Consider an aircraft with the following aerodynamic & mission specificat...

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Recap:

Consider an aircraft with the following aerodynamic & mission specification: 

  • CD0 = 0.0181; k = 1.23; AR = 8.9
  • Hold speed = 214 kts at 1500 ft
  • Rate of turn = 3.6 deg/s
  • Throttle setting 50%

  • Hold weight = 0.85 MTOW

Q4 What is the thrust factor (Thold/Tsls) at 1500 ft, to 3 d.p.?

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