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- Load factor and stalling speed are related in the following ways123:
- Load factor is the ratio of the lift force to the weight of the aircraft. It increases during maneuvers such as turns.
- Stalling speed increases with load factor. For example, 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's1.
- In a level, 60-degree-bank turn, the effective weight on the wings doubles, and stall speed increases by about 40 percent2.
- Stall speed increases at the square root of the load factor3.
Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.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… - People also ask
Why Does Stall Speed Increase With Bank Angle? | Boldmethod
When you turn, you need to increase your total lift to maintain altitude. You increase your total lift by increasing your angle of attack, which means you're closer to stall than you were in wings-level flight. And, your stall speed increases in proportion to the square root of your load factor. So the more you bank, at … See more
When you're flying straight and level, the lift that your wings produce points straight up, opposing gravity. But when you start to bank, that lift vector starts … See more
Let's say you enter a 30 degree banked turn and you don't change the amount of lift your wing is producing. In the banked turn, some of the lift that was keeping … See more
Another thing that happens in a constant altitude, coordinated turn is load factor. Load factor is measured in Gs. So if your load factor in a turn is 2 Gs, you feel twice … See more
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Since lift varies directly with the square of the airspeed, the increase in stall speed with bank angle can be shown to be directly related to the square root of the load factor, that is: …
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A speed of 1.7 times stalling speed (about 102 knots in a light aircraft with a stalling speed of 60 knots) produces a load factor of 3 Gs. Only a very narrow margin for error can be allowed for …
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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 …
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What is the stall speed at “Z” degrees angle of bank (bank angle suggests load factor)? A specific stall speed can be provided in response to each of these questions. Weight must be included …
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When the load factor of an aircraft increases above 1, the stall speed increases. As the load factor comes closer to 0, stall speed decreases and becomes "infinitely" low (basically 0 kts) …
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Since the load factor squares as the stalling speed doubles, it may be realized that tremendous loads may be imposed on structures by stalling an airplane at relatively high airspeeds. The …
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