| 190 |
 Profile drag coefficient increment due to full-span single-slotted flaps (Handley Page and NACA types). |
Aero F.02.01.06 |
| 190 |
Increment to C sub m sub zero due to flaps on swept-back wings. |
Aero F.08.01.02 |
| 190 |
Pitching moment coefficient increment due to flaps for unswept wings. |
Aero F.08.01.01 |
| 190 |
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of leading-edge high-lift devices. |
00029 |
| 190 |
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge double- and triple-slotted flaps at low speeds. |
99014 |
| 190 |
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge single-slotted flaps at low speeds. |
99004 |
| 190 |
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge plain flaps at low speeds. |
98017 |
| 190 |
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge split flaps, at low speeds. |
98009 |
| 190 |
Computer program for estimation of lift curve to maximum lift for wing-fuselage combinations with high-lift devices at low speeds. |
99031 |
| 190 |
Lift curve of wings with high-lift devices deployed at low speeds. |
96003 |
