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Physics, 12.03.2020 02:12 rama64

If the slope of the C versus CL curve is — 0.15 and the pitching moment at zero lift is equal to 0.08, determine the trim lift coefficient. If the center of gravity of the airplane is located at X, s/c = 0.3, determine the stick fixed neutral point.

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If the slope of the C versus CL curve is — 0.15 and the pitching moment at zero lift is equal to 0.0...

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