With an increase in the amount of flap deployment, the stalling angle of a wing
- increases.
- remains the same.
- decreases.
Explanation from PART66Online
Trailing-edge flaps increase camber, which raises the maximum lift coefficient but causes the airflow to separate at a lower angle of attack. As a result the stalling angle of the wing decreases as more flap is deployed. This is why deck-angle limits are reduced with flap extended.
B
boholbo asked · 23 Apr 2025
Please why is it not decrease,,,?
flap deploy -> flap stall speed decrease -> stall AOA also decrease..?
Community Comments (1)
C
cancaroman
3 May 2026
I agree with you, there's another question which Is saying that with flap deployment there's a decrease of aoa stall
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