ESDU 82017
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Yr)F , (Nr)F , (Lr)F
Abstract:
ESDU 82017 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to rate of yaw for aircraft at subsonic speeds. The data are applicable where there is a linear variation of lift coefficient with angle of attack and a linear variation of sideforce, yawing moment and rolling moment coefficients with angle of sideslip.Indexed under:
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