240 |
Stability derivative (L sub v) sub gamma. Contribution of full-span dihedral to rolling moment due to sideslip. |
Aero A.06.01.03 |
240 |
Pitching velocity derivatives for wings at supersonic speeds Z sub q and M sub q. |
Aero W.S.08.03.02 |
240 |
Pitching moment derivative due to rate of pitch for projectiles at supersonic speeds. |
91004 |
240 |
Pitching moment and lift force derivatives due to rate of pitch for aircraft at subsonic speeds. |
90010 |
240 |
Kinetic pressure in the wake behind a wing. |
Aero W.05.01.01 |
240 |
Effect of trailing-edge flap deployment on average downwash at the tailplane at low speeds. |
97021 |
240 |
Effect of twin fins on isolated tailplane lift-curve slope. |
91009 |
240 |
Installed tailplane lift-curve slope at subsonic speeds. |
89029 |
240 |
Lift and drag of two staggered lifting surfaces at low speeds. |
81023 |
240 |
Average downwash at the tailplane at low angles of attack and subsonic speeds. |
80020 |