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Normally, increasing the angle of attack between a wing and the airflow causes the lift
produced to increase. This can continue until a point is reached where maximum lift is generated and this is known as the
stall or stall angle. Any further increase in angle does not produce a corresponding increase in lift, and will
in fact lead to a sudden reduction in lift, a change in pitching moment or a wing drop.
This graph shows the typical behaviour of most airfoils:
Aerodynamic description of a stall
Stalling an aeroplane
An aeroplane can be made to stall by reducing the speed to the stall speed (which corresponds to the stall angle described
above) and attempting to prevent the plane from descending by applying inreasing up elevator control input. When an aeroplane
approaches the stall speed it has already adopted an extremely nose-high attitude, and the pilot will notice the controls have
become less responsive. The pilot may also notice some buffeting, an aerodynamic vibration caused by the airflow starting to
detach from the wing surface.
In most cases, as the stall is reached the aircraft will start to descend (because the wing is no longer producing enough lift
to support the aeroplane) and the nose will pitch down. Recovery from this stalled state usually involves the pilot lowering the
nose and increasing the speed, until normal flight can be resumed. The manoeuvre is normally quite safe and if correctly handled
leads to only a small loss of height. It is normally taught and practiced purely in order to help pilots recognise and avoid
it.
A special form of asymmetric stall in which the aircraft also rotates about its yaw axis is called a spin.
Stalling characteristics
Different aircraft types have different stalling characteristics. A benign stall is one where the nose drops gently and the
wings remain level throughout. Slightly more demanding is a stall where one wing stalls slightly before the other, causing that
wing to drop sharply, with the possibility of entering a spin. A
dangerous stall is one where the nose rises, pushing the wing deeper into the stalled state and potentially leading to an
unrecoverable deep stall.
Stall devices
Aeroplanes can be equipped with a variety of devices to prevent or postpone a stall or to make it less (or in some cases more)
severe, or to make recovery easier. A stall strip is a small sharp-edged device which, when attached to the
leading edge of a wing, encourages the stall to start there in preference to any other location on the wing. If attached close to
the wing root it makes the stall gentle and progressive; if attached near the wing tip it encourages the aircraft to drop a wing
when stalling. An anti-stall strake is a wing extension at the root leading edge which generates a vortex on the wing upper surface to postpone the stall. A stick-pusher is a
mechanical device which prevents the pilot from stalling an aeroplane by pushing the controls forwards as the stall is
approached. A stick-shaker is a similar device which shakes the pilot's controls to warn of the onset of stall.
A stall warning is an electronic or mechanical device which sounds an audible warning as the stall speed is
approached.
See Also
Alternately, a stall is a phenomenon whereby an internal combustion engine abruptly ceases operating and stops turning. The can happen
spontaneously (perhaps due to fuel starvation or a mechanical failure), or in response to a
sudden increase in engine load (perhaps due to incorrect manual transmission driving technique).
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