ESDU 82010:1993
$89.05
Contribution of fin to side force, yawing moment and rolling moment derivatives due to sideslip, (Y sub v) sub F, (N sub v) sub F, (L sub v) sub F, in the presence of body, wing and tailplane
Published By | Publication Date | Number of Pages |
ESDU | 1993-04-01 | 37 |
ESDU 82010 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to sideslip 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.