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  2. A wing stalls when12345:
    • The angle of attack increases beyond a critical point.
    • The airflow over the wing separates from the surface.
    • The lift coefficient decreases.
    • The wing loses its lift.
    • The airplane experiences increased air resistance and decreased lift.
    Learn more:
    Namely, the wing rapidly stops producing lift, and the airflow over the wing separates from the surface. The name for this is a stall. Regardless of how much further the pilot ‘pulls back,’ the wing still won’t produce much lift, which is then promptly exceeded by the force of weight (gravity).
    pilotinstitute.com/what-is-a-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-…
    At a specific angle of attack, called the critical angle of attack, air going over a wing will separate from the wing or "burble" (see figure 1), causing the wing to lose its lift (stall). The airspeed at which the wing will not support the airplane without exceeding this critical angle of attack is called the stalling speed.
    www.pilotfriend.com/training/flight_training/fxd_win…
    Stall is an undesirable phenomenon in which aircraft wings experience increased air resistance and decreased lift. It can cause an airplane to crash. Stall occurs when a plane is under too great an angle of attack (the angle of attack is the angle between the plane and the direction of flight).
    web1.eng.famu.fsu.edu/~dommelen/research/airfoil…
    The lift generated by a wing is dependent upon a smooth accelerated airflow over the the wing. At moderate angle of attack the airflow near the trailing edge of the wing become mildly turbulent. As the angle of attack increases, the turbulent air progresses forward toward the leading edge of the wing until the stalling angle is reached.
    www.studyflight.com/stall/
     
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