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    Stall (fluid dynamics) - Wikipedia

    In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases. This occurs when the critical angle of attack of the foil is exceeded. The critical angle of attack is typically about 15°, but it may vary significantly depending on the fluid, foil, and Reynolds number. … See more

    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 … See more

    Variation of lift with angle of attack image

    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 … See more

    Dynamic stall
    Dynamic stall is a non-linear unsteady aerodynamic effect that occurs when airfoils rapidly … See more

    Stall speeds image
    Overview image
    Types image

    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 … 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 … 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

     
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