In the video:
You describe how to set the equation for the NACA0015 wing profile.
Very nice. But one mistake about the Start value: strict 0 provides an error in function Sqrt([t])! Need to set Start with a near 0 value like 0.0001
In the video:
You describe how to set the equation for the NACA0015 wing profile.
Very nice. But one mistake about the Start value: strict 0 provides an error in function Sqrt([t])! Need to set Start with a near 0 value like 0.0001
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