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  2. In general terms, a stall is when an aircraft wing stops producing lift due to an excessive angle of attack. The angle of attack is the angle between the wings cord line and the oncoming airflow. The wing can be made to generate lift by reducing the angle of attack to an appropriate level.
    pilotinstitute.com/what-is-a-stall/
    A stall is a condition in aerodynamics and aviation such that if the angle of attack on an aircraft increases beyond a certain point, then lift begins to decrease. The angle at which this occurs is called the critical angle of attack.
    en.wikipedia.org/wiki/Stall_(fluid_dynamics)
    Definition of Stall In aviation, a stall is a condition in aerodynamics where an increase in the angle of attack leads to a reduction in the lift coefficient. This occurs when the critical angle of attack is exceeded, resulting in the airflow separating from the upper surface of the wing and a subsequent loss of lift.
    www.studyflight.com/understanding-the-dynamics-…
    A stall is an aerodynamic condition which occurs when smooth airflow over the airplane’s wings is disrupted, resulting in loss of lift. Specifically, a stall occurs when the AOA—the angle between the chord line of the wing and the relative wind—exceeds the wing’s critical AOA.
    flight-study.com/airplane-stalls/
    A stall is what happens when an aerofoil can not make enough lift to keep the aircraft in flight. Stalling can be risky and dangerous when caused unintentionally or with lack of enough vertical distance for recovery. Airflow separating from an airfoil at a high angle of attack, as occurs at a stall.
    simple.wikipedia.org/wiki/Stall_(flight)
     
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