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 = 0.0172; k = 1.23; AR = 7.6
- Cruise Mach = 0.84 at 34,000 ft
- Throttle setting 77%
- Cruise weight = 0.97 % MTOW
- Residual rate of climb allowance = 2.1 m/s
Q4 What is the cruise thrust factor (T/Tsls) at 34,000 ft, to 3 d.p.?
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