What is the stall angle of attack for the T-6?

The stall angle of attack for the T-6, which is essential for understanding its flight characteristics and safety margins, is indeed around 18 units. This angle represents the point at which the wing can no longer produce enough lift to support the aircraft's weight, leading to a stall.

At this angle of attack, airflow over the wing becomes turbulent, and lift significantly decreases. Pilots need to be aware of this threshold during flight operations, particularly during maneuvers that approach this angle. Flying at or beyond the stall angle can result in loss of control, which is why it's critical for pilots to understand this parameter for safe flying practices.

The stall angle of attack is influenced by various factors, including the airfoil design and wing configuration. In this case, the T-6's airfoil characteristics yield a stall angle near 18 units, making it an important number for training and operational knowledge.