def METHOD_NAME(self):
    self.initial_mesh.add_output("x_aero0", self.cruise.get_mesh())
    self.connect("initial_mesh.x_aero0", "geometry.x_aero_in")
    # create geometric DV setup
    self.geometry.nom_addVSPVariable("WingGeom", "XSec_1", "Root_Chord", scaledStep=False)
    self.geometry.nom_addVSPVariable("WingGeom", "XSec_2", "Root_Chord", scaledStep=False)
    self.geometry.nom_addVSPVariable("WingGeom", "XSec_3", "Root_Chord", scaledStep=False)
    self.geometry.nom_addVSPVariable("WingGeom", "XSec_4", "Root_Chord", scaledStep=False)
    self.geometry.nom_addVSPVariable("WingGeom", "XSec_4", "Tip_Chord", scaledStep=False)