Showing posts with the label equation of airfoilShow all
python airfoil
naca airfoil ploting in matplotlib python
Naca airfoil ploting in matplotlib python Code: from matplotlib.pyplot import * from numpy import * t = .2 c= 1.5 xc = linspace(0,1,100) y1 = t*c/.2*(.296*sqrt(xc)-.12…
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