peteroznewman
Subscriber
nYes, this is one reason why your lift and drag coefficients are way off.nThe Velocity Specification Method is not correct. The air is coming in normal to the semi-circle, that is directed toward the center of the circle where it collides with the wing.nYou want Components. You want the air coming in parallel to the X axis in a nice smooth air stream.nPut 20 m/s in the X component and 0 m/s in the Y component.n
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