0c2f54da0ae3e3802f1816ef45e81835007ca427,trunk/SUAVE/Components/Energy/Networks/Solar.py,Solar,evaluate_thrust,#Solar#,70

Before Change

        
        //Create the outputs
        F                                        = num_engines * F * [1,0,0]   
        F_mag                                    = np.atleast_2d(np.linalg.norm(F, axis=1)/Units.lbs) // lb   
        conditions.propulsion.disc_loading       = (F_mag.T)/ (num_engines*np.pi*(R/Units.feet)**2)   // lb/ft^2                     
        conditions.propulsion.power_loading      = (F_mag.T)/(P/Units.hp)                  // lb/hp 
        

After Change

        
        //Create the outputs
        F                                        = num_engines * F * [1,0,0]   
        F_mag                                    = np.atleast_2d(np.linalg.norm(F, axis=1))   
        conditions.propulsion.disc_loading       = (F_mag.T)/ (num_engines*np.pi*(R)**2) // N/m^2               
        conditions.propulsion.power_loading      = (F_mag.T)/(P)  // N/W                  
        

Instances