How does an increase in angle of attack affect the dynamic pressure and static pressure on the upper surface of an airfoil?

An increase in the angle of attack significantly influences the flow dynamics around an airfoil. As the angle of attack increases, the airflow over the upper surface accelerates, leading to a decrease in static pressure according to Bernoulli's principle. This occurs because, as the air speed increases, static pressure must drop to conserve energy within the flow.

Simultaneously, the dynamic pressure, which is associated with the velocity of the airflow (calculated as 0.5 * density * velocity^2), increases due to the heightened airspeed over the airfoil. The enhanced lift generated at greater angles of attack benefits from this rise in dynamic pressure, even though the static pressure drops.

Thus, the relationship here illustrates that with an increase in angle of attack, while static pressure decreases due to the acceleration of airflow, dynamic pressure inherently increases because the velocity of the air over the airfoil increases, leading to a combined effect that supports lift generation and affects overall aerodynamic performance.