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Excerpt from Propellers in Yaw
Equations (25) to (28) give the stability derivatives of single and dual - rotating propellers with respect to yaw, but the results are not yet in final form. There remain the evaluation of a', b', c', and d' and the introduction of a factor to account for the effect of a spinner and another factor to correct for the assumption of uniform loading of the side force over the propeller disk.
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