ESDU 82017 A
ESDU 82017 A 1983-JUL-01 Contrbuton of fn to sdeforce yawng moment and rollng moment dervatves due to rate of yaw Y sub r sub F N sub r sub F L sub r sub F
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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.