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 = 0.0178; k = 1.21; AR = 8.3
- Hold speed = 275 kts at 2000 ft
- Rate of turn = 2.6 deg/s
- Throttle setting 50%
Hold weight = 0.76 MTOW
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