During a turn, the stalling angle
- increases with bank angle.
- decreases noticeably.
- remains the same.
Explanation from PART66Online
The stalling angle of attack is a property of the aerofoil and is fixed regardless of manoeuvre. In a turn the increased load factor raises the stalling speed, so the wing reaches that same critical angle at a higher airspeed, but the angle itself does not change with bank.
M
manin asked · 21 May 2013
plz explan
Community Comments (2)
P
PART66Online
21 May 2013
Hey!
There is nothing to explain. Just a fact. But don't confuse stall angle and stall speed in turn. In turn stall speed will increase in factor of square root of load factor. V(stall in turn) = V(stall) * square_root(load factor). Load factor depends on roll angle.
There is nothing to explain. Just a fact. But don't confuse stall angle and stall speed in turn. In turn stall speed will increase in factor of square root of load factor. V(stall in turn) = V(stall) * square_root(load factor). Load factor depends on roll angle.
M
manin
24 May 2013
thanks
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