get_airfoil_camberΒΆ
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