Stalls
A stall occurs when a wing reaches its critical angle of attack.
Regardless of load factor, airspeed, bank angle, or atmospheric conditions, a wing always
stalls at the same critical angle of attack. Pilots control angle of attack with the
elevator.
A stall is an aerodynamic phenomenonit has nothing to do with an airplane's
engine. Gliders, huge airliners, jet fighters, and prop-driven, general aviation trainers
all stall when their wings reach a specific angle of attacknot because their engines
falter.
Anatomy of a Stall
Up to a point, increasing the angle of attack increases the amount of lift a wing
produces. Eventually, however, air flowing over the top of the wing can no longer follow
the wing's contour and it begins to swirl like water flowing over rocks in a stream. At
this point, called the critical angle of attack, total lift drops suddenly, and the wing
stalls.
Every wing has a specific critical angle of attack, and it always stalls at that angle.
Most general aviation aircraft have wings with a critical angle of attack of about 15
degrees.
Inexperienced pilots often mistake pitch attitude for angle of attack. Remember that
the airplane's flight path (and therefore the relative wind) may not be
in the direction that the nose of the airplane is pointing.
Warning Signs
A slight shaking or buffeting often precedes a stall. This vibration begins as the air
flowing over the top of the wing becomes turbulent. When this air hits the horizontal
stabilizer and elevator you may feel a slight vibration in the control yoke or stick. Most
airplanes have a stall warning horn to alert you as the airplane approaches a stall.
Recovering From a Stall
There is only one way to recover from a stallreduce the angle of attack. Apply
forward pressure on the control yoke or stick to reduce the angle of attack, and add power
to minimize loss of altitude.