| 170 |
 Normal force on flaps and controls. |
Aero F.05.01.01 |
| 170 |
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a double-slotted or triple-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds. |
94031 |
| 170 |
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a single-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds. |
94030 |
| 170 |
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a trailing-edge split flap, with or without a leading-edge high-lift device, at low speeds. |
94029 |
| 170 |
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a plain trailing-edge flap, with or without a leading-edge high-lift device, at low speeds. |
94028 |
| 170 |
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of various leading-edge high-lift devices at low speeds. |
94027 |
| 170 |
Introduction to the estimation of the lift coefficients at zero angle of attack and at maximum lift for aerofoils with high-lift devices at low speeds. |
94026 |
| 170 |
Fuselage interference effects on flap characteristics. |
97003 |
| 170 |
Information on the use of Data Items on high-lift devices. |
97002 |
| 170 |
Example of procedure in calculation of control hinge moments. |
89010 |
