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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 = 0.0174; k = 1.20; AR = 7.4
  • Cruise Mach = 0.86 at 34,000 ft
  • Throttle setting 75%

  • Cruise weight = 0.95 % MTOW
  • Residual rate of climb allowance = 0.8 m/s

Q4 What is the cruise thrust factor (T/Tsls) at 34,000 ft, to 3 d.p.?

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