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How can I calculate the angle of attack of an airfoil?

AOA is taken by gathering the arctangent of (w / u) or arctangent (v_z / v_x) Where w (or v_z) is the speed (velocity) of motion downwards (relative to the body) where up is positive [and of course, ...
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Variable-pitch propeller blade design (AOA)

A couple of important distinctions here: Angle of Attack (AoA) is the local angle of the blade profile relative to the airflow. Blade pitch is the local angle of the blade profile relative to the ...
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