Consider a single-engine piston-prop acrobatic aircraft with the following features: mro 1200 kg, S = 14...

 

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Consider a single-engine piston-prop acrobatic aircraft with the following features: mro 1200 kg, S = 14 m, P = 200 kW, b= 10, V = 60 knot (with flap), Cp=0.023, 1p = 0.75, e = 0.8. Evaluate the fastest turn performance (i.e., determine the maximum turn rate). Consider a single-engine piston-prop acrobatic aircraft with the following features: mro 1200 kg, S = 14 m, P = 200 kW, b= 10, V = 60 knot (with flap), Cp=0.023, 1p = 0.75, e = 0.8. Evaluate the fastest turn performance (i.e., determine the maximum turn rate).