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Principles of flight
The red arrows show the separation point, where the air can no longer follow the
curvature of the profile because the angle of attack becomes too high.
As the angle of attack increases, the separation point moves forward along the
wing, and eventually, the wing stalls, meaning it loses its lift.
5.3.6.3 Lift, speed, area
Doubling the wing area doubles the lift.
Doubling the speed quadruples the lift.
The same applies to drag.
The wing encounters twice as many
molecules moving at twice the speed.
If the angle of attack is not reduced, it will result in an increase in climb rate.
5.3.6.4 The critical angle of attack
As the angle of attack increases, lift also increases. If you, for example, double the
angle of attack, the lift will also double (assuming speed remains unchanged).
However, this only applies to angles of attack under about 12 degrees. See the
figure on the next page.
Many wing profiles generate lift at negative angles of attack. Lift increases almost
proportionally with an increase in angle of attack, up until the maximum lift is
reached.
Further increases in the angle of attack cause the wing to stall.
Flight Theory PPL(A)(UL)/LAPL Henning Andersen, Midtjysk Flyveskole© 2025 456