Question 16 The optimum angle of attack of an aerofoil is the angle at which a the lowest lift/drag ratio is produced Ob
Posted: Sun May 22, 2022 9:22 am
Question 16 The optimum angle of attack of an aerofoil is the angle at which a the lowest lift/drag ratio is produced Ob the highest lift/drag ratio is produced Oc the aerofoil produces zero lift Od the aerofoil produces maximum lift