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CAA NZ CPL Theory - Principles of Flight & Aircraft Performance

CAA NZ CPL Theory - Principles of Flight and Aircraft Performance (New Zealand)

AerodynamicsEnglish

Practice session

According to the lift equation L = 0.5 * rho * V^2 * S * CL, what occurs to total lift if airspeed (V) is doubled while angle of attack and air density remain constant?

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