def METHOD_NAME(path_to_case):
    case_name = path_to_case.split('/')[-1]
    pmor = configobj.ConfigObj(path_to_case + f'/{case_name}.pmor.sharpy')
    alpha = pmor['parameters']['alpha']
    inertial_forces = np.loadtxt(f'{path_to_case}/forces/forces_aeroforces.txt',
                                 skiprows=1, delimiter=',', dtype=float)[1:4]
    inertial_moments = np.loadtxt(f'{path_to_case}/forces/moments_aeroforces.txt',
                                  skiprows=1, delimiter=',', dtype=float)[1:4]
    return alpha, inertial_forces[2], inertial_forces[0], inertial_moments[1]