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Physics, 21.09.2019 04:30 gcristhian8863

Asmall drone has a straight wing with the following characteristics: wingspan 62", tip chord 6.25" fuselage chord 11.75". the width of the aircraft along the wing is constant and equal to 9 inches assume the trailing edge angle is zero. assume the wing extends through the fuselage. calculate: the chord as a function of y, c(y) (10 points) a. (5 points) the reference area b. the aspect ratio (5 points) d. mean aerodynamic chord (5 points) the location of the mean c. aerodynamic chord (5 points) the pitching moment about the center of pressure.

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Asmall drone has a straight wing with the following characteristics: wingspan 62", tip chord 6.25"...
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