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CG location effect on asymmetric yaw
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1st Jan 2021, 07:59
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washoutt
Join Date: Apr 2015
Location: Netherlands
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One thing I miss in the discussion is the gyroscopic effect due to engine rotation on yaw in flight. I was triggered by Gums remark on the need for rudder input in the case of TOGA with centerline thrust. Any thoughts on that?
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washoutt
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