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  2. An increase in angle of attack results in an increase in both lift and induced drag, up to a point. Too high an angle of attack (usually around 17 degrees) and the airflow across the upper surface of the aerofoil becomes detached, resulting in a loss of lift, otherwise known as a Stall.
    skybrary.aero/articles/angle-attack-aoa
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  3. People also ask
    What angle of attack does an aircraft stall at?The airspeed at which the aircraft stalls varies with the weight of the aircraft, the load factor, the center of gravity of the aircraft and other factors. However, the aircraft always stalls at the same critical angle of attack. The critical or stalling angle of attack is typically around 15° - 18° for many airfoils.
    What is the stalling angle of attack?The critical or stalling angle of attack is typically around 15° - 18° for many airfoils. Some aircraft are equipped with a built-in flight computer that automatically prevents the aircraft from increasing the angle of attack any further when a maximum angle of attack is reached, regardless of pilot input.
    Does a jet stall at the same angle of attack?The aircraft will always stall at the same angle of attack, called the critical angle. Many modern jets have an instrument that prevents the pilot from increasing the angle of attack past the critical angle, this is called the angle of attack limiter or alpha limiter.
    Why does a wing stall at the critical angle of attack?A wing stalls at the critical angle of attack. 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.
     
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