With an increase in the amount of flap deployment, the stalling angle of a wing
- remains the same.
- increases.
- decreases.
Explanation from PART66Online
Trailing-edge flaps increase camber, raising the maximum lift coefficient but causing the airflow to separate at a lower angle of attack. Consequently the stalling angle decreases as flap deployment increases, even though the stalling speed is reduced.
R
riccio_ruffo_44 asked · 11 Mar 2026
Can Someone axplane me why?
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