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- A stall in aircraft refers to12345:
- A sudden reduction in the lift generated by an aerofoil when the critical angle of attack is reached or exceeded.
- When an aircraft wing stops producing lift due to an excessive angle of attack.
- Occurs when the angle of attack of the wing is increased too much.
- Can be risky and dangerous when caused unintentionally or with lack of enough vertical distance for recovery.
- Results in decreased 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.Definition Stall is defined as a sudden reduction in the lift generated by an aerofoil when the critical angle of attack is reached or exceeded.skybrary.aero/articles/stallIn 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/So, what happens during a stall, and how does it happen? 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).simpleflying.com/airplane-stalls/A stall is what happens when an aerofoil can not make enough lift to keep the aircraft in flight. Stalling can be risky and dangerous when caused unintentionally or with lack of enough vertical distance for recovery. Airflow separating from an airfoil at a high angle of attack, as occurs at a stall.simple.wikipedia.org/wiki/Stall_(flight)A stall is a condition in aerodynamics and aviation wherein the angle of attack increases beyond a certain point such that the lift begins to decrease.www.spacesafetymagazine.com/aerospace-engine… - People also ask
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WEBA stall is a condition in aerodynamics and aviation wherein the angle of attack increases beyond a certain point such that the lift begins to decrease. The angle at which this occurs is called the critical angle of attack.
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