stopped running cg calculations

Author: jmvegh

Regional_Jet_Optimization/Optimize.py

@@ -24,7 +24,7 @@
 # ----------------------------------------------------------------------  
 def main():
     problem = setup()
-    
+    output = problem.objective()
     #uncomment these lines when you want to start an optimization problem from a different initial guess
     '''
     inputs                                   = [1.28, 1.38]

Regional_Jet_Optimization/Procedure.py

@@ -14,8 +14,8 @@
 from SUAVE.Analyses.Process import Process
 from SUAVE.Methods.Propulsion.turbofan_sizing import turbofan_sizing
 from SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry import compute_turbofan_geometry
-from SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity import compute_component_centers_of_gravity
-from SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity import compute_aircraft_center_of_gravity
+#from SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity import compute_component_centers_of_gravity
+#from SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity import compute_aircraft_center_of_gravity
 from SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff import compute_max_lift_coeff
 from SUAVE.Optimization.write_optimization_outputs import write_optimization_outputs
 
@@ -204,11 +204,11 @@ def weight(nexus):
     # weight analysis
     weights = nexus.analyses.base.weights.evaluate()
 
-    
+    '''
     compute_component_centers_of_gravity(vehicle)
     nose_load_fraction=.06
     compute_aircraft_center_of_gravity(vehicle,nose_load_fraction)
-   
+    '''
 
     weights = nexus.analyses.cruise.weights.evaluate()
     vehicle.mass_properties.breakdown = weights