when using Ansys to find the stall angle of a wing once the wing stalls the lift increases again, does anyone know why this is?
I did an experiment on the same wing in a wind tunnel and the same thing happened in my experimental data
Hi James,
Could you please specify the type of the wing, whether it is swept or not....and is it two or three dimensional??
Its wired. But never came across such thing in experimental stats. Looking forward for the update
The wing is a NACA0015 and it is in 2D, I varied the angle of attack by changing the direction of airflow and then resolving using trigonometry to find the true lift and drag. One theory I have is that potentially once the wing stalls it starts to act as a parachute and therefore causes a force perpendicular to thie wing which is interpreted to be lift. Aws Al-Akam
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