| 260 |
 Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of roll, (Y sub p) sub F, (N sub p) sub F, (L sub p) sub F, in the presence of body, wing and tailplane. |
83006 |
| 260 |
Contribution of wing planform to derivatives of yawing moment and sideforce due to roll rate at subsonic speeds (N sub p) sub w and (Y sub p) sub w. |
81014 |
| 260 |
Stability derivative L sub p, rolling moment due to rolling for swept and tapered wings. |
Aero A.06.01.01 |
| 260 |
Spanwise centre of pressure of isolated lifting surface at supersonic speeds. |
Aero A.S.06.03.04 |
| 260 |
Lift-curve slope of isolated lifting surface at supersonic speeds. |
Aero A.S.01.03.02 |
| 260 |
Computer program for prediction of aircraft lateral stability derivatives in sideslip at subsonic speeds. |
00025 |
| 260 |
Contribution of body-mounted fins and tailplanes to lateral derivatives due to sideslip at subsonic speeds for general body width to height ratio. |
93007 |
| 260 |
Contribution of ventral fins to sideforce and yawing moment derivatives due to sideslip at low angle of attack. |
92029 |
| 260 |
Contribution of fin and tailplane to sideforce and yawing moment derivatives due to sideslip at supersonic speeds at low angle of attack. |
91031 |
| 260 |
Lift-curve slope for single fin and rudder. (i) Body shape merging into fin. |
Aero C.01.01.01 |
