The
explanation of lift favored by this website
states that lift is created by an imbalance of pressure against a wing—lower
pressure on the top surface and higher pressure on the bottom surface. This
"pressure distribution" can be calculated accurately for both
subsonic and supersonic flight. But there are other ways of explaining how lift
is created.
Downwash
is especially noticeable beneath a helicopter's rotating blades.
Credit:
United Technologies Sikorsky Aircraft
According
to this explanation, the slight downward deflection of the air leaving the
trailing edge of a wing is what produces lift. Since for every action there is
an equal and opposite reaction, the downward push on the air must result in an
upward push on the wing. But this “downwash” results from air pressure differences
on the wing—it is an effect of lift, not the cause of it. The wing cannot
“feel” the airstream behind it being deflected downward; but it does feel the
pressure of air molecules colliding against its surface.
This
is the oldest and most complex theory of lift. It explains how the difference
in air speed over and under the wing results from a net “circulation” of air.
Above the wing, the circulatory flow adds to the overall speed of the air;
below the wing, it subtracts. But the actual force on the wing results from the
difference in air pressure caused by the difference in airflow speeds.