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  2. The stall angle in aviation refers to1234:
    • The angle of attack of an aerofoil exceeding the value which creates maximum lift.
    • When a wing exceeds the critical angle of attack.
    • The point where the air can no longer flow in contact with the upper surface of the wing.
    • An excessive angle of attack causing the wing to stop producing lift.
    Learn more:
    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. This angle varies very little in response to the cross section of the (clean) aerofoil and is typically around 15°.
    skybrary.aero/articles/stall
    A stall occurs when a wing exceeds the critical angle of attack. Factors that change the angle of attack include turning and changes in pitch. Recovering from a stall is possible by reducing the angle of attack and regaining airflow over the wing.
    simpleflying.com/angle-of-attack-airplane-stall-anal…
    Stall angle In aviation the stall angle is when the angle between the wing and the relative wind (due to the speed) is too great, the air can no longer flow in contact with the upper surface of the wing. Aerodynamically, laminar flow becomes turbulent flow.
    www.futura-sciences.us/dico/d/physics-stall-angle-…
    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/
     
  3. People also ask
    What is a stall in aviation?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.
    What is stall angle?This angle varies very little in response to the cross section of the (clean) aerofoil and is typically around 15°. At the stall, the airflow across the upper cambered surface ceases to flow smoothly and in contact with the upper surface and becomes turbulent, thus greatly reducing lift and increasing drag.
    Is a stall in an aircraft an angle of attack problem?The angle of attack at which the stall occurs is known as the critical angle of attack. This is the only factor that can result in a stall. Hence, a stall in an aircraft is an angle of attack problem. Get the latest aviation news straight to your inbox: Sign up for our newsletters today.
    What is stalling angle of attack?An aircraft's stalling speed is published by the manufacturer (and is required for certification by flight testing) for a range of weights and flap positions, but the stalling angle of attack is not published. As speed reduces, angle of attack has to increase to keep lift constant until the critical angle is reached.
     
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