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Aerodynamic Stall

Also known as:wing stallflow separationloss of lift

An aerodynamic stall occurs when the angle of attack of a wing exceeds the critical angle, causing boundary layer separation over most of the upper surface and a sudden, dramatic reduction in lift accompanied by a large increase in drag. It is not related to engine failure but is a purely aerodynamic phenomenon that can occur at any airspeed and any attitude. Recovery requires reducing angle of attack by lowering the nose, applying full power, and levelling wings — making stall recognition and recovery a core pilot training requirement.

Stall Speed for Representative Aircraft Under Different Load Conditions

Aircraft TypeMTOW (kg)Stall Speed Clean (km/h)Stall Speed Flaps (km/h)Wing Area (m²)
Cessna 172 (light trainer)1111978116.2
Boeing 737-80079016241213125.0
Airbus A380575000280250845.0
Piper PA-28 Cherokee1089917815.8
Eurofighter Typhoon2350020018550.0

Interactive Tools

NASA FoilSim III

Visualise flow separation and stall onset on an aerofoil

Open Tool

Khan Academy

Video lessons on stall, boundary layer, and flow separation

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Brilliant.org

Aerodynamics problem sets including stall and critical angle of attack

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Diagram showing boundary layer separation and stall on an aerofoil at high angle of attack

Wikimedia Commons, CC BY-SA

Related Terms

Engineering

Angle of Attack

The angle of attack (AoA) is the acute angle between the chord line of an aerofoil (or the longitudinal axis of a body) and the direction of the oncoming airflow (relative wind). It is one of the most critical parameters in aerodynamics, directly controlling the magnitude of lift and drag generated by a wing; increasing AoA raises lift up to a critical value beyond which the flow separates and the wing stalls. Pilots continuously manage angle of attack to balance lift against weight during all phases of flight.

Engineering

Aerodynamic Lift

Aerodynamic lift is the component of the net aerodynamic force acting perpendicular to the direction of the oncoming airflow, enabling aircraft, wings, and aerofoils to overcome gravity. It arises primarily from the pressure difference between the upper and lower surfaces of a wing, explained by Bernoulli's principle and the Kutta-Joukowski theorem. Lift is fundamental to fixed-wing flight and is carefully optimised in aircraft design through wing shape, angle of attack, and airspeed.

Engineering

Aerodynamics

Aerodynamics is the branch of fluid mechanics that studies the motion of air and other gases, and the forces they exert on solid bodies moving through them. It forms the scientific foundation for the design of aircraft, rockets, automobiles, and buildings, governing phenomena such as lift, drag, and pressure distribution. Understanding aerodynamic principles is essential for optimising vehicle performance, fuel efficiency, and structural stability at various speeds and altitudes.

The aeronautical use of "stall" to mean a loss of lift derives from the Old English steall (standing still, cessation of motion). It entered aviation vocabulary in the early 1910s as pilots experienced loss of control at high angles of attack.

stallboundary-layerflow-separationangle-of-attacklift-lossaviation-safety