get_airfoil_camber¶

get_airfoil_camber

Define the camber of an airfoil based on its coordinates

param n_points_camber:
param x:	x coordinates of the airfoil surface
type x:	np.array
param y:	y coordinates of the airfoil surface
type y:	np.array
	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