jb747
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- Mar 9, 2010
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When selecting various degrees of flaps during the periods when they are not fully retracted, do the controls automatically adjust the slats too? Can flaps and slats be controlled separately if required? When might this happen?
On older aircraft the leading and trailing edge devices could be controlled separately. Alternate modes of operation may still operate that way. But, normally, we just move the flap lever to a setting and the control is automatic.
Flaps are the devices at the trailing edge of the wing. They increase the curvature of the wing and in some cases also extend in such a way that the wing area is increased. They provide more lift and more drag.
At the leading edge of the wing you can have either leading edge flaps (747) or slats (380). A slat is a panel that does nothing other than create a large slot, through which air flows to help keep the boundary layer of air attached.
A flap increases the lift, but it will also decrease the angle of attack at which the wing stalls. A slat does little to the lift directly, but the slot will cause the wing to stall later, and at a greater angle of attack (and so generate more lift). On the airliners, slats are controlled, but on some aircraft (the A4G for instance) the slats were held in by air pressure and could extend as the flows changed. During the preflight, you could just push them in with one hand.