The geometry is the 15% Jukowski foil with camber, quantified by the height of the mean line at $x=0$, ie $\bar y = \frac 12 (y[N/4]+y[3N/4])$.
Compute the lift force coefficient $C_L$ and boundary layer separation point locations for $\bar y/c = 0.02,0.04,0.08$ at $\alpha=0$ using $N=128$ panels, and compare to the symmetric foil solution.
In [1]:
from IPython.core.display import HTML
def css_styling():
styles = open('../styles/custom.css', 'r').read()
return HTML(styles)
css_styling()
Out[1]: