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Engineering, 05.05.2020 04:21 javier1026

Consider a 2D airfoil with a zero lift angle of attack of −4 degrees. The stall angle for this airfoil is 15 degrees, where the maximum 2D lift coefficient is found to be 2.0. This airfoil is used in an aircraft with a non-elliptic wing of span 20m and planform area of 60 m2 . If 1 = 2 = 0.01, the weight of the plane is 105 Newton, density of air is 1 kg/m3 , find out the maximum landing speed that the plane can have

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Consider a 2D airfoil with a zero lift angle of attack of −4 degrees. The stall angle for this airfo...

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