Published in the October
1997 issue of Continental,
Continental Airlines' in-flight magazine
What Do Wing Flaps Do?
By Dave Esser
Modern jet transport aircraft have wings designed to
operate efficiently within a wide range of air speeds.
Transport aircraft must be able to fly at speeds of from
100 miles per hour to close to the speed of sound. A look
at the wing's secondary control surfaces -- flaps and
slats -- will explain how the highly adaptable wing accommodates
this range of speed.
Flaps are located on the aft or "trailing edge" of the
wing and increase both lift and drag. Because of the increased
drag, flaps are only partially extended on takeoff, and
fully extended on landing. The added drag created by full
flaps on landing allows the aircraft to approach at a
steep angle without excessive air speed. Think of a car
as it rolls downhill. If the hill is too steep, the car's
speed becomes excessive. By using the drag of the brakes,
the speed stays under control.
The greater the wing's camber, or curvature, the better
the wing will perform at slow air speeds. Flaps extend
downward and rearward, thereby increasing both camber
and wing area. The flaps extend in several segments, creating
gaps, known as slots, in the wing. The slots allow high
energy air from below the wing to vent over the top of
the wing. This high energy air "tricks the wing into thinking"
it is traveling faster than it actually is, enhancing
the low speed performance. On the leading edge of the
wing are the slats. As the slats extend forward another
slot is opened on the leading edge of the wing. The combination
of the slats and flaps creates an airfoil of significant
camber for low speed operations.
The wing is said to be "dirty" when the flaps and slats
are extended, referring to the high amount of drag the
wing experiences. In the dirty configuration the wing
is capable of low speed flight; the high drag would, however,
prohibit high speed flight. After takeoff the wing is
"cleaned up." After climbing through 400 feet the air
speed is allowed to increase, reducing the need for the
flaps and slats. After the completion of the flap and
slat retraction, the aircraft can accelerate to cruise
speed. During the approach for landing, the flaps and
slats are again extended. The flaps are set to an initial
setting, usually one degree. The leading edge slats are
later deployed. When initiating the final descent for
landing, the flaps are fully extended. Now that the wing
is again in its low speed configuration, the aircraft
can be slowed to its final approach speed.
Aircraft designers know that no wing is efficient at
all speeds. By using flaps, slats and slots, a wing can
take on beneficial low speed characteristics for takeoff
and landing, and characteristics beneficial for high speed
flight while at cruise. If it were not for flaps and slats,
the takeoff and landing speeds would have to be much greater
and runways would be prohibitively long.
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