'''Gianluca Mancini'''


# here necessary imports
import numpy as np


def basic_shear_flow(v_z, v_y, cross_sectional_property):

    ''' basic_shear_flow takes as input the
    shear forces in the z and y direction
     acting at the hinge in any point along the aileron

     The coordinate frame system for this calculations tilted at
    theta degrees with respect to the horizon line


     v_z = shear force in the z direction
     v_y = shear force in y direction
     booms = booms objects
     skin = skin objects
     izz = moment of inertia around z axis
     iyy = moment of inertia around y axis
     '''

    q_b=


