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A question for those who fly with fully articulated rotors
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8th Jul 2008, 03:39
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Overdrive
Join Date: Mar 2008
Location: England... what's left of it...
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If a rotor disc is unloaded in the sense of providing no lift or horizontal stability (due to negative g or otherwise), then I'd've thought the effect on the ship from the tail rotor would be no different irrespective of the rotor system?
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Overdrive
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