f8c1cb259cb3a5cab9907bb87f1522909ee852af,trunk/SUAVE/Analyses/Aerodynamics/SU2_inviscid.py,SU2_inviscid,evaluate,#SU2_inviscid#Any#Any#Any#,107

Before Change

            inviscid_lift[ii] = lift_model.predict([np.array([AoA[ii][0],mach[ii][0]])]) //sklearn fix
            
        conditions.aerodynamics.lift_coefficient                                 = inviscid_lift
        conditions.aerodynamics.lift_breakdown                                   = Data()
        conditions.aerodynamics.lift_breakdown.compressible_wings                = Data()
        conditions.aerodynamics.lift_breakdown.total                             = inviscid_lift        
        conditions.aerodynamics.lift_breakdown.compressible_wings["main_wing"]   = inviscid_lift // currently using vehicle drag for wing        
                                                                           

After Change

        state.conditions.aerodynamics.lift_breakdown.compressible_wings  = inviscid_lift
        
        // Inviscid drag, zeros are a placeholder for possible future implementation
        inviscid_drag                                              = np.zeros([data_len,1])       
        state.conditions.aerodynamics.inviscid_drag_coefficient    = inviscid_drag
        
        return inviscid_lift, inviscid_drag

Instances