get_airfoil_camber

get_airfoil_camber

Define the camber of an airfoil based on its coordinates

param x:

x coordinates of the airfoil surface

type x:

np.array

param y:

y coordinates of the airfoil surface

type y:

np.array

param n_points_camber:

number of points to define the camber line

type n_points_camber:

int

returns:

x coordinates of the camber line camber_y (np.array): y coordinates of the camber line

rtype:

camber_x (np.array)

Notes

The x and y vectors are expected in XFOIL format: TE - suction side - LE - pressure side - TE