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A stall is a (usually undesired) condition in aerodynamics and aviation.
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:
An aeroplane can be made to stall in any pitch or bank angle or at any airspeed but is commonly practiced by pilots reducing the speed to the stall speed. Stall speed varies on different airplanes and is represented by color codes on the air speed indicator. As the plane flies at this speed the angle of attack must be increased to prevent any loss of altitude or gain in airspeed (which corresponds to the stall angle described above). Any attempt to prevent the plane from descending by applying inreasing up elevator control input or increasing the airspeed by use of the throttle will cause the airplane to stall. When an aeroplane approaches the stall speed smooth air over the top and bottom of the wing no longer remains smooth causing the the relationship of high pressure below the wing and low pressure above the wing to lose its effect. The pilot will notice the flight controls have become less responsive and may also notice some buffeting, an aerodynamic vibration caused by the airflow starting to detach from the wing surface.
In most light aircraft, depending on the stability charactistics of the airplane, 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 decreasing the angle of attack and increasing the air speed, until smooth air flow over the wing is resumed. Normal flight can be resumed once recovery from the stall is complete. The maneuver is normally quite safe and if correctly handled leads to only a small amounts of loss in altitude. It is normally taught and practiced purely in order to help pilots recognize and avoid stalling the airplane in critical phases of flight such as landing and takeoff.
A special form of asymmetric stall in which the aircraft also rotates about its yaw axis is called a spin.
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.
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.
The majority of aircraft contain some form of device that warns the pilot of an impending stall. The simplest such device is a 'stall warning horn', which consists of either a pressure sensor or a moveable metal tab that detects the changes in airflow and produce an audible warning in response. Military aircraft often have an angle of attack indicator which lets the pilot know precisely how close to the stall point he is.
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).
A stall may also refer to:
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