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  2. A stall in aviation refers to1234:
    • When an aircraft wing stops producing lift due to an excessive angle of attack.
    • It occurs when smooth airflow over the airplane’s wings is disrupted, resulting in loss of lift.
    • Specifically, a stall occurs when the angle between the chord line of the wing and the relative wind exceeds the wing’s critical angle.
    • If the angle of attack increases beyond a certain point, lift begins to decrease, and this angle is called the critical angle of attack.
    Learn more:
    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/
    Stall is defined as a sudden reduction in the lift generated by an aerofoil when the critical angle of attack is reached or exceeded.
    skybrary.aero/articles/stall
    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 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)
     
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