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- A wing stalls when the angle of attack exceeds a certain point, called the critical angle of attack1234. At this point, the air going over the wing separates from the wing or "burble", causing the wing to lose its lift1. The lift generated by a wing is dependent upon a smooth accelerated airflow over the wing, and as the angle of attack increases, the airflow near the trailing edge of the wing becomes mildly turbulent, progressing forward toward the leading edge of the wing until the stalling angle is reached2. Once a wing stalls, it rapidly stops producing lift, and the airflow over the wing separates from the surface5.Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.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…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/A stall is a condition in aerodynamics and aviation wherein the angle of attack increases beyond a certain point such that the lift begins to decrease. The angle at which this occurs is called the critical angle of attack. Air flow separation begins to occur at small angles of attack while attached flow over the wing is still dominant.www.spacesafetymagazine.com/aerospace-engine…A stall occurs when the angle of attack of an aerofoil exceeds the value which creates maximum lift as a consequence of airflow across it. Changing the effective configuration of a wing by the deployment of leading edge or trailing edge devices will directly alter the angle of attack at which an aerofoil stalls.mull-overthing.com/where-do-rectangular-wings-st…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/
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