An aircraft weighs 120 kN and it has a maximum coefficient of lift of 1.47. Its drag equation is given by: Cp = 0.03 +0.043 C? How much drag will the aircraft create is it flies at stall speed with lift equal to weight?
An aircraft weighs 120 kN and it has a maximum coefficient of lift of 1.47. Its drag equation is given by: Cp = 0.03 +0.043 C? How much drag will the aircraft create is it flies at stall speed with lift equal to weight?
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Transcribed Image Text:An aircraft weighs 120 kN and it has a maximum coefficient of lift of 1.47. Its drag equation is
given by:
Cp = 0.03 +0.043 C?
How much drag will the aircraft create is it flies at stall speed with lift equal to weight?
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