Doing so, the forward wing lift reduces the downward force the horizontal stabilizer needs to produce - reducing the amount of lift the main wing must produce.

Turning can be described as 'climbing around a circle' (wing lift is diverted to turning the aircraft) so the increase in wing angle of attack creates even more drag.

A crash of flak made the wing lift.

We may analyse the longitudinal static stability by considering the aircraft in equilibrium under wing lift, tail force, and weight.

For a symmetrical airfoil at low angle of attack, the wing lift is proportional to the angle of attack:

Due to the air launch and wing lift, the first-stage flight algorithm is custom-designed.

Experimentally Segnbora raised an arm, and was dumbfounded to see the serrated shape of a Dragon's wing lift away from the shadow-body.

With a rolling vertical landing the aircraft uses downward jet thrust to hover while it is still moving fast enough to also generate wing lift.

The wing lift achieves two essentials effects:

Although it is true that the air moving over the top of a wing generating lift does move faster, there is no requirement for equal transit time.