| 250 |
 Contribution of tailplane-mounted twin fins to sideforce, yawing moment and rolling moment derivatives due to sideslip. |
92007 |
| 250 |
Estimation of sideforce and yawing moment derivatives due to sideslip for complete aircraft at subsonic speeds. |
82011 |
| 250 |
Contribution of fin to sideforce, 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. |
82010 |
| 250 |
Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. |
81032 |
| 250 |
Effect of trailing-edge flaps on sideforce and yawing moment derivatives due to sideslip, (Y sub v) sub f and (N sub v) sub f. |
81013 |
| 250 |
Effect of trailing-edge flaps on rolling moment derivative due to sideslip, (L sub v) sub f. |
80034 |
| 250 |
Contribution of wing planform to rolling moment derivative due to sideslip, (L sub v) sub w, at subsonic speeds. |
80033 |
| 250 |
Wing-body yawing moment and sideforce derivatives due to sideslip: N sub v and Y sub v (with Addendum A for nacelle effects). |
79006 |
| 250 |
Effects of isolated body and wing-body interference on rolling moment due to sideslip: L sub v (with Addendum A for nacelle effects). |
73006 |
| 250 |
Stability derivative (L sub v) sub gamma. Contribution of part-span dihedral to rolling moment due to sideslip. |
Aero A.06.01.09 |
