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  2. A study of this effect has revealed that the airplane's stalling speed increases in proportion to the square root of the load factor. This means that an airplane with a normal unaccelerated stalling speed of 50 knots can be stalled at 100 knots by inducing a load factor of 4 G's.
    avstop.com/AC/FlightTraingHandbook/loadfactorsa…
    Stall speed increases as weight increases, since wings need to fly at a higher angle of attack to generate enough lift for a given airspeed. The increase in load factor in a turn also increases stall speed; in a level, 60-degree-bank turn, for instance, the effective weight on the wings doubles and stall speed increases by about 40 percent.
    www.aopa.org/news-and-media/all-news/2020/mar…
    Regardless of the type of airplane, the load factor increases at a predictable rate. At 45 degrees of bank in a level turn, for example, the load factor is 1.4, meaning gravity will feel 40 percent stronger. The biggest impact of load factor is on stall speed. It increases at the square root of the load factor.
    www.aopa.org/news-and-media/all-news/2016/sept…
     
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  7. WEBOct 28, 2019 · Load on an aircraft is stress, and load factor is the ratio of lift to weight. Load factor (G’s) = Lift / Weight. Hence in level flight, where a 2,000 pound aircraft is creating 2,000 pounds of lift, the aircraft is …

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