5.2 Consider the following aircraft flying in straight and level unaccelerated trimmed flight at M = 0.2 at sea level. L
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5.2 Consider the following aircraft flying in straight and level unaccelerated trimmed flight at M = 0.2 at sea level. L
5.2 Consider the following aircraft flying in straight and level unaccelerated trimmed flight at M = 0.2 at sea level. L Mac 12A Хер W x = 0.5cwing M = 0 M = -5000 ft·lb T = 3000 lb W = 12,000 lb Cwing = 8 ft Ctail = 4 ft bwing = 30 ft = DOL e=1 Зо, = 0 deg AR, = 7.65 AR, = 5 = -2 deg Sw= 240 ft? S, = 40 ft? (a) What is the trimmed angle of attack of the tail? (b) What is the trimmed angle of attack of the wing?
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