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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/sThrottle setting 50%
Hold weight = 0.85 MTOW
Answer the following three questions in turn:
Q1 What is the density of the atmosphere at the hold altitude, in kg/m3 , to 4 d.p.?
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