80154aa1808d74a48ef50f7e002d564e02a4d93f,trunk/SUAVE/Analyses/Aerodynamics/Vortex_Lattice.py,Vortex_Lattice,evaluate,#Vortex_Lattice#Any#Any#Any#,75

Before Change

        for wing in geometry.wings.values():
            // run vortex lattice at quaried flight conditions
            [wing_lift,wing_lift_coeff,wing_drag,wing_drag_coeff] = weissinger_vortex_lattice(conditions,settings,wing,propulsors)
            conditions.aerodynamics.lift_breakdown.inviscid_wings_lift[wing] = inviscid_wings_lift[wing]
            state.conditions.aerodynamics.lift_coefficient_wing[wing]        = inviscid_wings_lift[wing]
               
            // lift 
            total_lift_coeff += wing_lift_coeff * wing.areas.reference / vehicle_reference_area

After Change

        

        // inviscid lift of wings only
        inviscid_wings_lift                                              = Data()
        //wing_lift_coeff = 0
        //wing_lift       = 0
        //wing_drag       = 0
        //wing_drag_coeff = 0

Instances