Aerodynamic Stall

An aerodynamic stall is a condition where an aerofoil exceeds its critical angle of attack, resulting in a sudden reduction in lift. This occurs because the smooth boundary layer separates from the upper surface of the wing, creating chaotic, turbulent airflow.

Key Points

• •Occurs when the <strong>critical angle of attack</strong> is exceeded, regardless of the aircraft's airspeed or weight.
• •Symptoms generally include buffeting, decreased control effectiveness, and a high rate of descent.
• •Primary recovery involves reducing the angle of attack, typically by applying forward pressure on the controls.

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