0c2f54da0ae3e3802f1816ef45e81835007ca427,trunk/SUAVE/Components/Energy/Networks/Battery_Propeller.py,Battery_Propeller,evaluate_thrust,#Battery_Propeller#,71

Before Change

        // Create the outputs
        F                                           = num_engines* F * [np.cos(self.thrust_angle),0,-np.sin(self.thrust_angle)]      
        mdot                                        = np.zeros_like(F) 
        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 
        
        results = Data()
        results.thrust_force_vector = F

After Change

        // Create the outputs
        F                                           = num_engines* F * [np.cos(self.thrust_angle),0,-np.sin(self.thrust_angle)]      
        mdot                                        = np.zeros_like(F) 
        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 
        
        results = Data()
        results.thrust_force_vector = F

Instances