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In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack exceeds its critical value.
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Сва́ливание в авиации — резкое падение подъёмной силы в результате нарушения нормальных условий обтекания крыла воздушным потоком. В условиях нормального обтекания крыла потоком воздуха создается достаточная подъёмная сила, и самолёт ведёт себя... Википедия
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.
11 апр. 2022 г. · 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 ...
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 ...
The stall is a breakdown of the smooth airflow over the wing into a turbulent one, resulting in a decrease in lift.
13 июл. 2022 г. · A stall occurs when a wing exceeds the critical angle of attack. The critical angle of attack is the AOA at which the wing generates the most ...
An airplane stall is a reduction in lift that occurs when the wing exceeds its critical angle of attack, disrupting airflow and decreasing lift.
2 янв. 2024 г. · A stall is a rapid decrease in lift caused by the separation of airflow from the wing's surface, brought on by exceeding the critical angle of attack.
This article briefly reviews the awareness and avoidance of aerodynamic wing stalls with particular reference to modern multi-engine public transport aircraft.
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