The results obtained by xfoi-python are different from those obtained by xfoil

DARcorporation / xfoil-python

Stripped down version of XFOIL as compiled python module

GNU General Public License v3.0

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The results obtained by xfoi-python are different from those obtained by xfoil #27

Open Karl-Liu-ch opened 7 months ago

Karl-Liu-ch commented 7 months ago

I'm trying to calculate the drag coefficient, but the same parameters give different results in xfoil and xfoil-python. airfoil-2.0_0.7.txt Re = 400000, alfa = 0.0. The cd obtained from xfoil is 0.00519, while the cd obtained from xfoil-python is 0.0033630472607910633.