The
size and shape of the wing, the angle at which it meets the oncoming air, the speed
at which it moves through the air, even the density of the air, all affect the
amount of lift a wing creates. Let’s begin with the shape of a wing intended
for subsonic flight.
Air
divides smoothly around a wing’s rounded leading edge, and flows neatly off its
tapered trailing edge. You might think a sharp leading edge would be better.
However, air cannot turn a sharp corner, so tilting a sharp wing even slightly
would disrupt the smooth airflow over the wing. This would cause a loss of lift
and increase drag. A rounded leading edge divides the airflow smoothly, even as
the wing is tilted up or down.
If
the trailing edge were rounded, the higher-pressure air flowing along the lower
side would try to follow the rounded surface and spill upward into the
lower-pressure air above the wing. A sharp trailing edge prevents this upward
spill, because air cannot make a sharp turn. Instead, the air flowing off the
top and bottom surfaces rejoins smoothly.
Tilting
the wing upward increases lift—to a point. If you tilt it too much, the airflow
pulls away from the upper surface, and the smooth flow turns turbulent. The
wing suddenly loses lift, a condition known as a stall. You can reestablish a smooth airflow by tilting the wing back
to a more level position.
Credit: Bill Tinkler
Flaps
change a wing’s curvature, increasing lift. Airplanes use flaps to maintain
lift at lower speeds, particularly during takeoff and
landing. This allows an airplane to make a slower landing approach and a
shorter landing. Flaps also increase drag, which helps slow the airplane and
allows a steeper landing approach.
The
Museum’s Jet
Aviation gallery contains a working model of a Lockheed L-1011 jetliner wing. It
demonstrates how the wing’s complex system of ailerons, flaps, and other
devices works during a landing.