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Fenster schliessen

A geometric twist of a wing is characterized by: 

Geometric chord profiles in subsequent sections do not lie in one plane.

Tips of wings are twistet down when speed is equal to 0.

Tips of wings are curved up during in flight.

On the tips od the wings there are airfoils, where the separated airflow leaving the wing for Absolute Angle of Attack (Absolute AoA) is less intense.

Fenster schliessen

Increasing the unit loading of the planform area causes: 

Take off and landing distance extending- increase of minimal speed (Vs)- decrease in maximal climbing rate(RoCmax).

Take off and landing distance - increse in minimal speed(Vs) - decrease in maximal climbing rate(RoCmax).

Take off and landing distance extending - decrease of minimal speed(Vs) - decrease in maximal climbing rate(RoCmax).

Take off and landing distance extending - increase in minimal speed(Vs) - increase in maximal climbing rate(RoCmax).