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  2. 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.
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    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-…
    Aerodynamic stall occurs when the angle of attack, pitch, or attitude becomes too large, causing lift to suddenly decrease. Stall recovery requires reorienting the aircraft so that its attack angle is low enough for lift to be restored. When the attack angle is high, flow separation will occur and will create a shear region with high pressure.
    resources.system-analysis.cadence.com/blog/msa…
    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…
    The term “aerodynamic stall” or simply “stall” is used to describe a situation in which the airflow around the aircraft wings is no longer smoothly following the wing shape as intended. Specifically, flow above the wing separates away from the wing surface, causing relatively large regions of recirculating and turbulent flow.
    www.flexcompute.com/blog/2022/03/31/aerodynam…
     
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    Stall (fluid dynamics) - Wikipedia

    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. If the angle of attack increases beyond the critical value, the lift decreases and the … See more

    In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack exceeds its critical value. The critical angle of attack is typically about 15°, but it may vary significantly depending on the See more

    Stalls depend only on angle of attack, not airspeed. However, the slower an aircraft flies, the greater the angle of attack it needs to produce lift … See more

    The normal stall speed, specified by the VS values above, always refers to straight and level flight, where the load factor is equal to 1g. … See more

    Fixed-wing aircraft can be equipped with devices to prevent or postpone a stall or to make it less (or in some cases more) severe, or to make recovery easier.
    • An aerodynamic twist can be introduced to the wing with the leading edge near the wing tip twisted … See more

    The graph shows that the greatest amount of lift is produced as the critical angle of attack is reached (which in early-20th century aviation was called the "burble point"). This angle is 17.5 degrees in this case, but it varies from airfoil to airfoil. In particular, for … See more

    Fixed-wing aircraft
    A fixed-wing aircraft can be made to stall in any pitch attitude or bank angle or at any airspeed but deliberate stalling is commonly practiced by reducing the speed to the unaccelerated stall speed, at a safe altitude. … See more

    Dynamic stall
    Dynamic stall is a non-linear unsteady aerodynamic effect that occurs when airfoils rapidly change the angle of attack. The rapid change can cause a strong vortex to be shed from the leading edge of the aerofoil, and … See more

     
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