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Physics, 06.03.2020 07:09 A1A2T3

Perform the tasks listed below for the wing of the SBJ (App. A). The wing planform extends from the fuselage centerline to the outside of the tip tanks. Starting from the measured values for the root chord, the tip chord, the span, and the sweep angle of the quarter chord line (App. A) calculate the planform area, the aspect ratio, the taper ratio, and the sweep of the leading edge. Also, calculate the length of the mean aerodynamic chord.

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Perform the tasks listed below for the wing of the SBJ (App. A). The wing planform extends from the...
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