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Question 2: Consider a rectangular wing of span b and chord c. ... | Filo
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the rectangular wing model of 40 in by 5 in has the following characteristics e087 a009 per degree and zero angle of attack at 3 degrees if a full scale rectangular wing of 42 ft by 6 ft is 75699
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Answered: Problem 1: Consider a flying wing with a NACA 2412 airfoil, an aspect atio of 10, and a wing area of 20 m2. Assume the span efficiency factor e =e= .9, and the… | bartleby
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A finite wing of area 1.5 ft^2 and aspect ratio of 6 is tested in a subsonic wind tunnel at a velocity of 130 ft / s at standard sea-level conditions. At an angle of attack of -1^∘, the measured lift and drag are 0 and 0.181 lb, respectively. At an angle of attack of 2^∘, the lift and drag are measured as 5.0 and 0.23 lb, respectively. Calculate the span efficiency factor and the infinite-wing lift slope. | Numerade
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