added Kraftwerk_class to combine multiple turbines
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@@ -1,3 +1,4 @@
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import numpy as np
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#importing Druckrohrleitung
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import sys
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import os
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@@ -8,12 +9,106 @@ from functions.pressure_conversion import pressure_conversion
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from Turbinen.Turbinen_class_file import Francis_Turbine
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class Kraftwerk_class:
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g = 9.81
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def __init__(self):
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self.turbines = []
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self.n_turbines = 0
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# setter
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def set_LAs(self,LA_vec,display_warning=True):
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for i in range(self.n_turbines):
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self.turbines[i].set_LA(LA_vec[i],display_warning)
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def set_pressure(self,pressure):
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for i in range(self.n_turbines):
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self.turbines[i].set_pressure(pressure)
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def set_steady_state(self,ss_flux,ss_pressure):
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self.identify_Q_proportion()
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for i in range(self.n_turbines):
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self.turbines[i].set_steady_state(ss_flux*self.Q_prop[i],ss_pressure)
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# getter
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def get_current_Q(self):
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Q = 0
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for i in range(self.n_turbines):
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Q += self.turbines[i].get_current_Q()
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return Q
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def get_current_LAs(self):
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LAs = []
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for i in range(self.n_turbines):
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LAs.append(self.turbines[i].get_current_LA())
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return np.array(LAs)
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def get_current_pressure(self):
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pressures = []
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for i in range(self.n_turbines):
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pressures.append(self.turbines[i].get_current_pressure())
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return np.array(pressures) # consider taking the average, after evaluating how the converge() method affects the result
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def get_n_turbines(self):
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return self.n_turbines
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def get_info(self):
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for turbine in self.turbines:
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turbine.get_info(full=True)
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# methods
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def identify_Q_proportion(self):
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Q_n_vec = np.zeros(self.n_turbines)
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for i in range(self.n_turbines):
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Q_n_vec[i] = self.turbines[i].get_Q_n()
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self.Q_prop = Q_n_vec/np.sum(Q_n_vec)
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def add_turbine(self,turbine):
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self.turbines.append(turbine)
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self.n_turbines += 1
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def update_LAs(self,LA_soll_vec):
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for i in range(self.n_turbines):
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self.turbines[i].update_LA(LA_soll_vec[i])
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def converge(self,convergence_parameters):
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# small numerical disturbances (~1e-12 m/s) in the velocity can get amplified at the turbine node, because the new velocity of the turbine and the
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# new pressure from the forward characteristic are not perfectly compatible.
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# Therefore, iterate the flux and the pressure so long, until they converge
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eps = 1e-12 # convergence criterion: iteration change < eps
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iteration_change = 1. # change in Q from one iteration to the next
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i = 0 # safety variable. break loop if it exceeds 1e6 iterations
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g = self.g # gravitational acceleration
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p = convergence_parameters[0] # pressure at second to last node (see method of characterisctics - boundary condidtions)
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v = convergence_parameters[1] # velocity at second to last node (see method of characterisctics - boundary condidtions)
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D = convergence_parameters[2] # diameter of the pipeline
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area_pipe = convergence_parameters[3] # area of the pipeline
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alpha = convergence_parameters[4] # elevation angle of the pipeline
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f_D = convergence_parameters[5] # Darcy friction coefficient
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c = convergence_parameters[6] # pressure wave propagtation velocity
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rho = convergence_parameters[7] # density of the liquid
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dt = convergence_parameters[8] # timestep of the characteristic method
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Q_old = self.get_current_Q()
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v_old = Q_old/area_pipe
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while iteration_change > eps:
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p_new = p-rho*c*(v_old-v)+rho*c*dt*g*np.sin(alpha)-f_D*rho*c*dt/(2*D)*abs(v)*v
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self.set_pressure(p_new)
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Q_new = self.get_current_Q()
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v_new = Q_new/area_pipe
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iteration_change = abs(Q_old-Q_new)
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Q_old = Q_new.copy()
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v_old = v_new.copy()
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i = i+1
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if i == 1e6:
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print('did not converge')
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break
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# print(i)
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def print_info(self):
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for turbine in self.turbines:
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turbine.get_info(full=True)
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