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- A stall in aviation occurs when1234:
- The angle of attack of an aircraft's wing increases too much.
- The critical angle of attack is exceeded.
- The airflow separates from the upper surface of the wing.
- There is a subsequent loss of lift.
Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.Namely, the wing rapidly stops producing lift, and the airflow over the wing separates from the surface. The name for this is a stall. Regardless of how much further the pilot ‘pulls back,’ the wing still won’t produce much lift, which is then promptly exceeded by the force of weight (gravity).pilotinstitute.com/what-is-a-stall/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.en.wikipedia.org/wiki/Stall_(fluid_dynamics)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.www.studyflight.com/understanding-the-dynamics-…Put simply, a stall is a reduction of lift experienced by an aircraft. It occurs when the angle of attack of the wing is increased too much. This is known as the critical angle of attack and is typically around 15 degrees (but there are variations). In normal flight, the airflow over the shaped wings creates lift.simpleflying.com/airplane-stalls/ - People also ask
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