An airplane has a total mass of 35,000 kg and a wing planform area of 65 m

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An airplane has a total mass of 35,000 kg and a wing planform area of 65 m2. The airplane is cruising at 10,000 m altitude with a velocity of 1100 km/h. The density of air on cruising altitude is 0.414 kg/m3. The lift coefficient of this airplane at the cruising altitude is

(a) 0.273 

(b) 0.290 

(c) 0.456 

(d) 0.874 

(e) 1.22

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