| 270 |
 Estimation of sideforce, yawing moment and rolling moment derivatives due to rate of yaw for complete aircraft at subsonic speeds. |
84002 |
| 270 |
Contribution of body to yawing moment and sideforce derivatives due to rate of yaw, (N sub r) sub B and (Y sub r) sub B. |
83026 |
| 270 |
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F. |
82017 |
| 270 |
Effect of wing on rolling moment due to yawing. |
72021 |
| 270 |
Aero-normalised stability derivatives: effect of wing on yawing moment due to yawing. |
71017 |
| 270 |
Stability derivative L sub p. Rolling moment due to rolling for radial multi-planar wing arrangements at supersonic speeds. |
Aero A.S.06.03.03 |
| 270 |
Stability derivative L sub p. Effect of fuselage interference on rolling moment due to rolling at supersonic speeds. |
Aero A.S.06.03.02 |
| 270 |
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds. |
Aero A.S.06.03.01 |
| 270 |
Estimation of sideforce, yawing moment and rolling moment derivatives due to rate of roll for complete aircraft at subsonic speeds. |
85010 |
| 270 |
Contribution of wing dihedral to sideforce, yawing moment and rolling moment derivatives due to rate of roll at subsonic speeds, (Y sub p) sub gamma, (N sub p) sub gamma and (L sub p) sub gamma. |
85006 |
