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Lift and Drag are not calculated

Hello all

I’ve been trying to analyze this airfoil with a round trailing edge, but everytime I go into the Airfoil Analysis Module it shows nothing after analysis, not sure what is going on. I’m attaching the screenshots and the airfoil file, if anyone can help me I would be so thankful.



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it seems that the trailing edge of your airfoil is closed. XFoil required a trailing edge gap.

Try to remove a few points at the trailing edge so that it is open. I also would not recommend simulating a rounded trailing edge in XFoil.