示例#1
0
 def _Pwsat(self, T):
     """Calculate the partial pressure of water in saturated moint air"""
     if T < 273.15:
         Pws = _Sublimation_Pressure(T)
     else:
         Pws = _PSat_T(T)
     return Pws
示例#2
0
文件: plots.py 项目: yfq000/iapws
    print("Calculating isochor lines...")
    for v in isov:
        print("    v=%s" % v)
        pts = [iapws.IAPWS95(T=t, v=v) for t in Tl]
        x = []
        y = []
        for p in pts:
            if p.status:
                x.append(p.__getattribute__(xAxis))
                y.append(p.__getattribute__(yAxis))
        plt.plot(x, y, **isov_kw)

# Plot region limits
if regionBoundary:
    # Boundary 1-3
    Po = _PSat_T(623.15)
    P = np.linspace(Po, 100, points)
    pts = [fluid(P=p, T=623.15) for p in P]
    x = [p.__getattribute__(xAxis) for p in pts]
    y = [p.__getattribute__(yAxis) for p in pts]
    plt.plot(x, y, **isosat_kw)

    # Boundary 2-3
    T = np.linspace(623.15, 863.15)
    P = [_P23_T(t) for t in T]
    P[-1] = 100  # Avoid round problem with value out of range > 100 MPa
    pts = [fluid(P=p, T=t) for p, t in zip(P, T)]
    x = [p.__getattribute__(xAxis) for p in pts]
    y = [p.__getattribute__(yAxis) for p in pts]
    plt.plot(x, y, **isosat_kw)
    def __init__(self, hp, ip, lp, m1, m2, m3, ma, steam_high_temp, water_low_temp):
        # Input Parameters
        self.HP = hp  # Bar
        self.IP = ip   # Bar
        self.LP = lp    # Bar

        mass_flow_1 = m1
        mass_flow_2 = m2
        mass_flow_3 = m3
        mass_flow_amine = ma

        self.massflows = {
            'mass flow 1': mass_flow_1,
            'mass flow 2': mass_flow_2,
            'mass flow 3': mass_flow_3,
            'mass flow to amine': mass_flow_amine
        }

        # total mass flow
        total_mass_flow = mass_flow_1 + mass_flow_2 + mass_flow_3

        # Turbine Mass Flows
        HPT_mass_flow = mass_flow_3
        IPT_mass_flow = HPT_mass_flow + mass_flow_2
        LPT_mass_flow = IPT_mass_flow + mass_flow_1 - mass_flow_amine

        # Pump Mass Flows
        HPP_mass_flow = mass_flow_3
        IPP_mass_flow = mass_flow_2
        LPP_mass_flow = IPP_mass_flow + HPP_mass_flow + mass_flow_1

        # HRSG Mass Flows
        self.economiser_1_mass_flow = total_mass_flow
        self.economiser_2_mass_flow = mass_flow_2
        self.economiser_3_mass_flow = mass_flow_3

        self.evaporator_1_mass_flow = mass_flow_1
        self.evaporator_2_mass_flow = mass_flow_2
        self.evaporator_3_mass_flow = mass_flow_3

        self.superheater_1_mass_flow = mass_flow_1 - mass_flow_amine
        self.superheater_2_mass_flow = mass_flow_2 + mass_flow_3
        self.superheater_3_mass_flow = mass_flow_3

        self.SteamHighTemp = steam_high_temp  # Celcius

        WaterLowTemp = water_low_temp  # Celcius

        quality = 0.9  # at turbine outlet

        self.T = [0]*16

        self.T[1] = ToKelvin(WaterLowTemp)

        # Pressures
        self.P = [0]*16
        self.P[1] = steam._PSat_T(self.T[1])

        # low pressure
        self.P[2] = BarToMP(self.LP)  # bar
        self.P[3] = self.P[2]
        self.P[4] = self.P[2]
        self.P[5] = self.P[2]

        # intermediate pressure
        self.P[7] = BarToMP(self.IP)  # bar
        self.P[8] = self.P[7]
        self.P[9] = self.P[8]
        self.P[10] = self.P[9]
        self.P[15] = self.P[9]

        # High Pressure
        self.P[11] = BarToMP(self.HP)  # bar
        self.P[12] = self.P[11]
        self.P[13] = self.P[12]
        self.P[14] = self.P[13]

        # Temperatures in kelvin

        self.T[3] = steam._TSat_P(self.P[3])
        self.T[4] = self.T[3]

        self.T[6] = self.T[1]

        self.T[8] = steam._TSat_P(self.P[8])
        self.T[9] = self.T[8]

        self.T[12] = steam._TSat_P(self.P[12])
        self.T[13] = self.T[12]
        self.T[14] = ToKelvin(self.SteamHighTemp)

        # Begin going around cycle working out available values
        self.SpecificValues = [0] * 16

        self.SpecificValues[1] = steam._Region1(self.T[1], self.P[1])

        self.T[2] = steam._Backward1_T_Ps(self.P[2], self.SpecificValues[1]['s'])
        self.SpecificValues[2] = steam._Region1(self.T[2], self.P[2])

        self.SpecificValues[3] = steam._Region4(self.P[3], 0)
        self.SpecificValues[4] = steam._Region4(self.P[3], 1)

        self.SpecificValues[6] = steam._Region4(self.P[1], quality)
        self.T[5] = steam._Backward2_T_Ps(self.P[5], self.SpecificValues[6]['s'])
        self.SpecificValues[5] = steam._Region2(self.T[5], self.P[5])

        self.T[7] = steam._Backward1_T_Ps(self.P[7], self.SpecificValues[3]['s'])
        self.SpecificValues[7] = steam._Region1(self.T[7], self.P[7])
        self.SpecificValues[8] = steam._Region4(self.P[8], 0)
        self.SpecificValues[9] = steam._Region4(self.P[8], 1)
        self.T[10] = steam._Backward2_T_Ps(self.P[10], self.SpecificValues[5]['s'])
        self.SpecificValues[10] = steam._Region2(self.T[10], self.P[10])
        self.T[11] = steam._Backward1_T_Ps(self.P[11], self.SpecificValues[3]['s'])
        self.SpecificValues[11] = steam._Region1(self.T[11], self.P[11])
        self.SpecificValues[12] = steam._Region4(self.P[12], 0)
        self.SpecificValues[13] = steam._Region4(self.P[13], 1)
        self.SpecificValues[14] = steam._Region2(self.T[14], self.P[14])
        self.T[15] = steam._Backward2_T_Ps(self.P[15], self.SpecificValues[14]['s'])
        self.SpecificValues[15] = steam._Region2(self.T[15], self.P[15])

        self.s = [0] * 16
        self.h = [0] * 16

        for i in range(0, len(self.SpecificValues)):
            if i == 0:
                continue
            self.s[i] = self.SpecificValues[i]['s']
            self.h[i] = self.SpecificValues[i]['h']

        #Printing T-P conditions at each point
        print("-------------------------------------------------------")
        print("\nCycle Conditions:")
        for i in range(1, 16):
            print("\n\tT"+str(+i)+" = "+str(ToCelcius(self.T[i]))+" C")
            print("\tP"+str(+i)+" = "+str(MPToBar(self.P[i]))+" bar")

        #Finding specific work of turbines and pump
        self.total_works = {
            'Work Type': 'Work [kW]',
            'LP Pump work': LPP_mass_flow * (self.h[2] - self.h[1]),
            'IP Pump work': IPP_mass_flow * (self.h[7] - self.h[3]),
            'HP Pump work': HPP_mass_flow * (self.h[11] - self.h[3]),
            'HP Turbine work': HPT_mass_flow * (self.h[14] - self.h[15]),
            'IP Turbine work': IPT_mass_flow * (self.h[10] - self.h[5]),
            'LP Turbine work': LPT_mass_flow * (self.h[5] - self.h[6]),
            'LP Superheater Heat Input': self.superheater_1_mass_flow * (self.h[5] - self.h[4]),
            'LP Evaporator Heat Input': self.evaporator_1_mass_flow * (self.h[4] - self.h[3]),
            'LP Economiser Heat Input':  self.economiser_1_mass_flow * (self.h[3] - self.h[2]),
            'IP Superheater Heat Input': self.superheater_2_mass_flow * (self.h[10] - self.h[15]),
            'IP Superheater 2 Heat Input': self.evaporator_2_mass_flow * (self.h[15] - self.h[9]),
            'IP Evaporator Heat Input': self.evaporator_2_mass_flow * (self.h[9] - self.h[8]),
            'IP Economiser Heat Input':  self.economiser_2_mass_flow * (self.h[8] - self.h[7]),
            'HP Superheater Heat Input': self.superheater_3_mass_flow * (self.h[14] - self.h[13]),
            'HP Evaporator Heat Input': self.evaporator_3_mass_flow * (self.h[13] - self.h[12]),
            'HP Economiser Heat Input':  self.economiser_3_mass_flow * (self.h[12] - self.h[11])
        }

        print("\nCycle Specific Works:")
        for work, value in self.total_works.items():
            print("\n\t"+work+" = "+str(value))

        #Finding Total Heat into Cycle from HRSG
        self.q_in = self.total_works['LP Economiser Heat Input'] + self.total_works['LP Evaporator Heat Input'] + self.total_works['LP Superheater Heat Input'] + self.total_works['IP Economiser Heat Input'] + \
            self.total_works['IP Evaporator Heat Input'] + self.total_works['IP Superheater Heat Input'] + self.total_works['HP Economiser Heat Input'] + self.total_works['HP Evaporator Heat Input'] + self.total_works['HP Superheater Heat Input']

        #FInding Net Work
        self.w_net = self.total_works['HP Turbine work'] + self.total_works['IP Turbine work'] + self.total_works['LP Turbine work'] - self.total_works['HP Pump work'] - self.total_works['IP Pump work'] - self.total_works['LP Pump work']
        self.total_works['Net Work'] = self.w_net
        #Finding Thermal Efficiency fo Steam Cycle
        self.efficiency = self.w_net / self.q_in
        self.total_works['Efficiency'] = self.efficiency

        print("\nCycle Efficiency:")
        print("\n\tefficiency = "+str(self.efficiency*100)+"%")
        print("\n\tWith a Net Work of : "+str(np.round(self.w_net))+"kW")
        print("\n\tand a Total Heat Input of: "+str(np.round(self.q_in))+"kW\n")
示例#4
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    def __alpha_tn_func(self, temp, params):
        import math
        import scipy.misc as diff
        import scipy.constants as unit
        import iapws.iapws97 as steam
        import iapws.iapws95 as steam2

        pressure = steam._PSat_T(temp)

        d_rho = steam2.IAPWS95(P=pressure, T=temp - 1).drhodT_P

        #d_rho2 = diff.derivative(derivative_helper, temp) # dRho/dTm

        rho = 1 / steam._Region4(pressure, 0)['v']  # mass density, kg/m3

        Nm = ((rho * unit.kilo) / params['mod molar mass']) * unit.N_A * (
            unit.centi)**3  # number density of the moderator
        d_Nm = ((d_rho * unit.kilo) / params['mod molar mass']) * unit.N_A * (
            unit.centi)**3  #dNm/dTm
        d_Nm = d_Nm * unit.zepto * unit.milli

        mod_macro_a = params[
            'mod micro a'] * Nm  # macroscopic absorption cross section of the moderator
        mod_macro_s = params[
            'mod micro s'] * Nm  # macroscopic scattering cross section of the moderator

        F = params['fuel macro a'] / (params['fuel macro a'] + mod_macro_a
                                      )  # thermal utilization, F
        #dF/dTm
        d_F = -1 * (params['fuel macro a'] * params['mod micro a'] *
                    d_Nm) / (params['fuel macro a'] + mod_macro_a)**2

        # Resonance escape integral, P
        P = math.exp(
            (-1 * params['n fuel'] *
             (params['fuel_volume']) * params['I']) / (mod_macro_s * 3000))
        #dP/dTm
        d_P = P * (-1 * params['n fuel'] * params['fuel_volume'] *
                   unit.centi**3 * params['mod micro s'] *
                   d_Nm) / (mod_macro_s * 3000 * unit.centi**3)**2

        Eth = 0.0862 * temp  # convert temperature to energy in MeV
        E1 = mod_macro_s / math.log(
            params['E0'] /
            Eth)  # neutron thermalization macroscopic cross section

        Df = 1 / (3 * mod_macro_s *
                  (1 - params['mod mu0']))  # neutron diffusion coefficient
        tau = Df / E1  # fermi age, tau
        #dTau/dTm
        d_tau = ((
            (0.0862 *
             (Eth / params['E0'])) * 3 * Nm) - math.log(params['E0'] / Eth) *
                 (params['mod micro s'] * d_Nm)) / ((3 * Nm)**2 *
                                                    (1 - params['mod mu0']))

        L = math.sqrt(1 / (3 * mod_macro_s * mod_macro_a *
                           (1 - params['mod mu0'])))  # diffusion length L
        # dL/dTm
        d_L = 1 / (2 * math.sqrt(
            (-2 * d_Nm * unit.zepto * unit.milli) /
            (3 * params['mod micro s'] * params['mod micro a'] *
             (Nm * unit.zepto * unit.milli)**3 * (1 - params['mod mu0']))))

        # left term of the numerator of the moderator temperature feedback coefficient, alpha
        left_1st_term = d_tau * (
            params['buckling']**2 + L**2 * params['buckling']**4
        )  #holding L as constant
        left_2nd_term = d_L * (
            2 * L * params['buckling']**2 + 2 * L * tau * params['buckling']**4
        )  # holding tau as constant
        left_term = (P * F) * (left_1st_term + left_2nd_term
                               )  # combining with P and F held as constant

        # right term of the numerator of the moderator temperature feedback coefficient, alpha

        right_1st_term = (-1) * (1 + ((tau + L**2) * params['buckling']**2) +
                                 tau * L**2 * params['buckling']**4
                                 )  # num as const
        right_2nd_term = F * d_P  # holding thermal utilization as constant
        right_3rd_term = P * d_F  # holding resonance escpae as constant
        right_term = right_1st_term * (right_2nd_term + right_3rd_term
                                       )  # combining all three terms together

        # numerator and denominator
        numerator = left_term + right_term
        denominator = params['eta'] * params['epsilon'] * (F * P)**2

        alpha_tn = numerator / denominator

        alpha_tn = alpha_tn / 3
        return alpha_tn
示例#5
0
文件: plots.py 项目: jjgomera/iapws
    for v in isov:
        print("    v=%s" % v)
        pts = [iapws.IAPWS95(T=t, v=v) for t in Tl]
        x = []
        y = []
        for p in pts:
            if p.status:
                x.append(p.__getattribute__(xAxis))
                y.append(p.__getattribute__(yAxis))
        plt.plot(x, y, **isov_kw)


# Plot region limits
if regionBoundary:
    # Boundary 1-3
    Po = _PSat_T(623.15)
    P = np.linspace(Po, 100, points)
    pts = [fluid(P=p, T=623.15) for p in P]
    x = [p.__getattribute__(xAxis) for p in pts]
    y = [p.__getattribute__(yAxis) for p in pts]
    plt.plot(x, y, **isosat_kw)

    # Boundary 2-3
    T = np.linspace(623.15, 863.15)
    P = [_P23_T(t) for t in T]
    P[-1] = 100  # Avoid round problem with value out of range > 100 MPa
    pts = [fluid(P=p, T=t) for p, t in zip(P, T)]
    x = [p.__getattribute__(xAxis) for p in pts]
    y = [p.__getattribute__(yAxis) for p in pts]
    plt.plot(x, y, **isosat_kw)
def plot(**kwargv):
    ###############################################################################
    # Configuration section
    ###############################################################################
    show = True

    # Define standard to use in plot, IAPWS95 very slow!
    fluid = iapws.IAPWS97
    # fluid = iapws.IAPWS95

    # Define kind of plot
    xAxis = "s"
    yAxis = "P"

    if "x" in kwargv:
        xAxis = kwargv["x"]
    if "y" in kwargv:
        yAxis = kwargv["y"]
    if "show" in kwargv:
        show = kwargv["show"]

    print("Calculating %s-%s Diagram..." % (yAxis, xAxis))

    # Point count for line, high value get more definition but slow calculate time
    points = 50

    # Saturation line format
    isosat_kw = {"ls": "-", "color": "black", "lw": 1}

    # Isoquality lines to plot
    isoq = np.arange(0.1, 1, 0.1)
    isoq_kw = {"ls": "--", "color": "black", "lw": 0.5}
    labelq_kw = {"size": "xx-small", "ha": "right", "va": "center"}

    # Isotherm lines to plot, values in ºC
    isoT = [0, 50, 100, 200, 300, 400, 500, 600, 700, 800, 1200, 1600, 2000]
    isoT_kw = {"ls": "-", "color": "red", "lw": 0.5}
    labelT_kw = {"size": "xx-small", "ha": "right", "va": "bottom"}

    # Isobar lines to plot
    isoP = [Pt, 0.001, 0.01, 0.1, 1, 10, 20, 50, 100]
    isoP_kw = {"ls": "-", "color": "blue", "lw": 0.5}
    labelP_kw = {"size": "xx-small", "ha": "center", "va": "center"}

    # Isoenthalpic lines to plot
    isoh = np.arange(200, 4400, 200)
    isoh_kw = {"ls": "-", "color": "green", "lw": 0.5}
    labelh_kw = {"size": "xx-small", "ha": "center", "va": "center"}

    # Isoentropic lines to plot
    isos = [1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
    isos_kw = {"ls": "-", "color": "brown", "lw": 0.5}
    labels_kw = {"size": "xx-small", "ha": "center", "va": "center"}

    # # Isochor lines to plot
    # isov = [0.1, 1, 10, 100]
    # isov_kw = {"ls": "-", "color": "green", "lw": 0.5}

    # Show region limits
    regionBoundary = False
    if "regionBoundary" in kwargv:
        regionBoundary = kwargv["regionBoundary"]

    # Show region5
    region5 = False

    ###############################################################################
    # Calculate
    ###############################################################################

    # Set plot label
    title = {
        "T": "T, K",
        "P": "P, MPa",
        "v": "v, m³/kg",
        "h": "h, kJ/kg",
        "s": "s, kJ/kgK"
    }

    # Check axis correct definition
    validAxis = ", ".join(title.keys())
    if xAxis not in title:
        raise ValueError("X axis variable don´t supported, valid only ",
                         validAxis)
    if yAxis not in title:
        raise ValueError("Y axis variable don´t supported, valid only ",
                         validAxis)
    if xAxis == yAxis:
        raise ValueError("X and Y axis can't show same variable")

    # Set plot legend
    plt.title("%s-%s Diagram" % (yAxis, xAxis))
    xtitle = title[xAxis]
    plt.xlabel(xtitle)
    ytitle = title[yAxis]
    plt.ylabel(ytitle)

    # Set logaritmic scale if apropiate
    if xAxis in ["P", "v"]:
        plt.xscale("log")
    if yAxis in ["P", "v"]:
        plt.yscale("log")
    plt.grid(True)

    # Calculate point of isolines
    Ps = list(
        np.concatenate([
            np.logspace(np.log10(Pt), np.log10(0.1 * Pc), points),
            np.linspace(0.1 * Pc, 0.9 * Pc, points),
            np.linspace(0.9 * Pc, 0.99 * Pc, points),
            np.linspace(0.99 * Pc, Pc, points)
        ]))
    Pl = list(
        np.concatenate([
            np.logspace(np.log10(Pt), np.log10(0.1 * Pc), points),
            np.linspace(0.1 * Pc, 0.5 * Pc, points),
            np.linspace(0.5 * Pc, 0.9 * Pc, points),
            np.linspace(0.9 * Pc, 0.99 * Pc, points),
            np.linspace(0.99 * Pc, Pc, points),
            np.linspace(Pc, 1.01 * Pc, points),
            np.linspace(1.01 * Pc, 1.1 * Pc, points),
            np.linspace(1.1 * Pc, 50, points),
            np.linspace(50, 100, points)
        ]))
    Tl = list(
        np.concatenate([
            np.linspace(0, 25, points),
            np.linspace(25, 0.5 * Tc, points),
            np.linspace(0.5 * Tc, 0.9 * Tc, points),
            np.linspace(0.9 * Tc, Tc, points),
            np.linspace(Tc, 1.1 * Tc, points),
            np.linspace(1.1 * Tc, 1.1 * Tc, points),
            np.linspace(1.1 * Tc, 800, points),
            np.linspace(800, 2000, points)
        ]))

    # Calculate saturation line
    print("Calculating saturation lines...")
    liq = [fluid(P=p, x=0) for p in Ps]
    xliq = [l.__getattribute__(xAxis) for l in liq]
    yliq = [l.__getattribute__(yAxis) for l in liq]
    plt.plot(xliq, yliq, **isosat_kw)
    vap = [fluid(P=p, x=1) for p in Ps]
    xvap = [v.__getattribute__(xAxis) for v in vap]
    yvap = [v.__getattribute__(yAxis) for v in vap]
    plt.plot(xvap, yvap, **isosat_kw)

    # Calculate isoquality lines
    print("Calculating isoquality lines...")
    Q = {}
    for q in isoq:
        Q["%s" % q] = {}
        txt = "x=%s" % q
        print("    %s" % txt)
        pts = [fluid(P=p, x=q) for p in Ps]
        x = [p.__getattribute__(xAxis) for p in pts]
        y = [p.__getattribute__(yAxis) for p in pts]
        Q["%s" % q]["x"] = x
        Q["%s" % q]["y"] = y
        plt.plot(x, y, **isoq_kw)

    # Calculate isotherm lines
    if xAxis != "T" and yAxis != "T":
        print("Calculating isotherm lines...")
        T_ = {}
        for T in isoT:
            T_["%s" % T] = {}
            print("    T=%sºC" % T)
            # Calculate the saturation point if available
            if T + 273.15 < Tc:
                liqsat = fluid(T=T + 273.15, x=0)
                vapsat = fluid(T=T + 273.15, x=1)
                sat = True
            else:
                sat = False
            pts = []
            for p in Pl:
                try:
                    point = fluid(P=p, T=T + 273.15)
                    if fluid == iapws.IAPWS97 and not region5 and \
                            point.region == 5:
                        continue
                    # Add saturation point if neccesary
                    if sat and T + 273.15 < Tc and point.s < vapsat.s:
                        pts.append(vapsat)
                        pts.append(liqsat)
                        sat = False
                    pts.append(point)
                except NotImplementedError:
                    pass
            x = []
            y = []
            for p in pts:
                if p.status:
                    x.append(p.__getattribute__(xAxis))
                    y.append(p.__getattribute__(yAxis))
            plt.plot(x, y, **isoT_kw)
            T_["%s" % T]["x"] = x
            T_["%s" % T]["y"] = y

    # Calculate isobar lines
    if xAxis != "P" and yAxis != "P":
        print("Calculating isobar lines...")
        P_ = {}
        for P in isoP:
            print("    P=%sMPa" % P)
            P_["%s" % P] = {}
            # Calculate the saturation point if available
            if P < Pc:
                liqsat = fluid(P=P, x=0)
                vapsat = fluid(P=P, x=1)
                sat = True
            else:
                sat = False
            pts = []
            for t in Tl:
                try:
                    point = fluid(P=P, T=t + 273.15)
                    if fluid == iapws.IAPWS97 and not region5 and \
                            point.region == 5:
                        continue
                    # Add saturation point if neccesary
                    if sat and P < Pc and point.status and point.s > vapsat.s:
                        pts.append(liqsat)
                        pts.append(vapsat)
                        sat = False
                    pts.append(point)
                except NotImplementedError:
                    pass

            x = []
            y = []
            for p in pts:
                if p.status:
                    x.append(p.__getattribute__(xAxis))
                    y.append(p.__getattribute__(yAxis))
            plt.plot(x, y, **isoP_kw)
            P_["%s" % P]["x"] = x
            P_["%s" % P]["y"] = y

    # Calculate isoenthalpic lines
    if xAxis != "h" and yAxis != "h":
        print("Calculating isoenthalpic lines...")
        H_ = {}
        for h in isoh:
            print("    h=%skJ/kg" % h)
            H_["%s" % h] = {}
            pts = []
            for p in Pl:
                try:
                    point = fluid(P=p, h=h)
                    if fluid == iapws.IAPWS97 and not region5 and \
                            point.region == 5:
                        continue
                    pts.append(point)
                except NotImplementedError:
                    pass
            x = []
            y = []
            for p in pts:
                if p.status:
                    x.append(p.__getattribute__(xAxis))
                    y.append(p.__getattribute__(yAxis))
            plt.plot(x, y, **isoh_kw)
            H_["%s" % h]["x"] = x
            H_["%s" % h]["y"] = y

    # Calculate isoentropic lines
    if xAxis != "s" and yAxis != "s":
        print("Calculating isoentropic lines...")
        S_ = {}
        for s in isos:
            print("    s=%skJ/kgK" % s)
            S_["%s" % s] = {}
            pts = []
            for p in Pl:
                try:
                    point = fluid(P=p, s=s)
                    if fluid == iapws.IAPWS97 and not region5 and \
                            point.region == 5:
                        continue
                    pts.append(point)
                except NotImplementedError:
                    pass
            x = []
            y = []
            for p in pts:
                if p.status:
                    x.append(p.__getattribute__(xAxis))
                    y.append(p.__getattribute__(yAxis))
            plt.plot(x, y, **isos_kw)
            S_["%s" % s]["x"] = x
            S_["%s" % s]["y"] = y

    # # Calculate isochor lines
    # if xAxis != "v" and yAxis != "v":
    # print("Calculating isochor lines...")
    # for v in isov:
    # print("    v=%s" % v)
    # pts = [fluid(P=p, v=v) for p in Pl]
    # x = []
    # y = []
    # for p in pts:
    #     if p.status:
    #         x.append(p.__getattribute__(xAxis))
    #         y.append(p.__getattribute__(yAxis))
    # plt.plot(x, y, **isov_kw)

    # Plot region limits
    if regionBoundary:
        # Boundary 1-3
        Po = _PSat_T(623.15)
        P = np.linspace(Po, 100, points)
        pts = [fluid(P=p, T=623.15) for p in P]
        x = [p.__getattribute__(xAxis) for p in pts]
        y = [p.__getattribute__(yAxis) for p in pts]
        plt.plot(x, y, **isosat_kw)

        # Boundary 2-3
        T = np.linspace(623.15, 863.15)
        P = [_P23_T(t) for t in T]
        P[-1] = 100  # Avoid round problem with value out of range > 100 MPa
        pts = [fluid(P=p, T=t) for p, t in zip(P, T)]
        x = [p.__getattribute__(xAxis) for p in pts]
        y = [p.__getattribute__(yAxis) for p in pts]
        plt.plot(x, y, **isosat_kw)

    # Show annotate in plot
    xmin, xmax = plt.xlim()
    ymin, ymax = plt.ylim()
    for q in isoq:
        x = Q["%s" % q]["x"]
        y = Q["%s" % q]["y"]

        txt = "x=%s" % q
        i = 0
        j = i + 1

        if xAxis in ["P", "v"]:
            fx = (log(x[i]) - log(x[j])) / (log(xmax) - log(xmin))
        else:
            fx = (x[i] - x[j]) / (xmax - xmin)
        if yAxis in ["P", "v"]:
            fy = (log(y[i]) - log(y[j])) / (log(ymax) - log(ymin))
        else:
            fy = (y[i] - y[j]) / (ymax - ymin)
        rot = atan(fy / fx) * 360 / 2 / pi
        plt.annotate(txt, (x[i], y[i]), rotation=rot, **labelq_kw)

    if xAxis != "T" and yAxis != "T":
        for T in isoT:
            x = T_["%s" % T]["x"]
            y = T_["%s" % T]["y"]

            if not x:
                continue

            txt = "%sºC" % T
            i = 0
            j = i + 2

            if xAxis in ["P", "v"]:
                fx = (log(x[i]) - log(x[j])) / (log(xmax) - log(xmin))
            else:
                fx = (x[i] - x[j]) / (xmax - xmin)
            if yAxis in ["P", "v"]:
                fy = (log(y[i]) - log(y[j])) / (log(ymax) - log(ymin))
            else:
                fy = (y[i] - y[j]) / (ymax - ymin)
            rot = atan(fy / fx) * 360 / 2 / pi
            plt.annotate(txt, (x[i], y[i]), rotation=rot, **labelT_kw)

    if xAxis != "P" and yAxis != "P":
        for P in isoP:
            x = P_["%s" % P]["x"]
            y = P_["%s" % P]["y"]

            if not x:
                continue

            txt = "%sMPa" % P
            i = len(x) - 15
            j = i - 2

            if xAxis in ["P", "v"]:
                fx = (log(x[i]) - log(x[j])) / (log(xmax) - log(xmin))
            else:
                fx = (x[i] - x[j]) / (xmax - xmin)
            if yAxis in ["P", "v"]:
                fy = (log(y[i]) - log(y[j])) / (log(ymax) - log(ymin))
            else:
                fy = (y[i] - y[j]) / (ymax - ymin)
            rot = atan(fy / fx) * 360 / 2 / pi
            plt.annotate(txt, (x[i], y[i]), rotation=rot, **labelP_kw)

    if xAxis != "h" and yAxis != "h":
        for h in isoh:
            x = H_["%s" % h]["x"]
            y = H_["%s" % h]["y"]

            if not x:
                continue
            if h % 1000:
                continue

            txt = "%s J/g" % h
            i = points
            j = i + 2

            if xAxis in ["P", "v"]:
                fx = (log(x[i]) - log(x[j])) / (log(xmax) - log(xmin))
            else:
                fx = (x[i] - x[j]) / (xmax - xmin)
            if yAxis in ["P", "v"]:
                fy = (log(y[i]) - log(y[j])) / (log(ymax) - log(ymin))
            else:
                fy = (y[i] - y[j]) / (ymax - ymin)
            rot = atan(fy / fx) * 360 / 2 / pi
            plt.annotate(txt, (x[i], y[i]), rotation=rot, **labelh_kw)

    if xAxis != "s" and yAxis != "s":
        for s in isos:
            x = S_["%s" % s]["x"]
            y = S_["%s" % s]["y"]

            txt = "%s J/gK" % s
            i = len(x) // 2
            if s > 10:
                j = i + 1
            else:
                j = i + 5

            if xAxis in ["P", "v"]:
                fx = (log(x[i]) - log(x[j])) / (log(xmax) - log(xmin))
            else:
                fx = (x[i] - x[j]) / (xmax - xmin)
            if yAxis in ["P", "v"]:
                fy = (log(y[i]) - log(y[j])) / (log(ymax) - log(ymin))
            else:
                fy = (y[i] - y[j]) / (ymax - ymin)
            rot = atan(fy / fx) * 360 / 2 / pi
            plt.annotate(txt, (x[i], y[i]), rotation=rot, **labels_kw)
    if show:
        plt.show()
示例#7
0
    def __alpha_tn_func(self, temp, params):
        pressure = steam._PSat_T(temp) # vfda: why accessing protected method?

        d_rho = steam2.IAPWS95(P=pressure, T=temp-1).drhodT_P

        rho = 1 / steam._Region4(pressure, 0)['v'] # mass density, kg/m3

        n_m = ((rho * unit.kilo)/self.mod_molar_mass) * unit.N_A * (unit.centi)**3
        # number density of the moderator
        d_nm = ((d_rho * unit.kilo)/self.mod_molar_mass) * unit.N_A * (unit.centi)**3 #dNm/dTm
        d_nm = d_nm * unit.zepto * unit.milli

        mod_macro_a = self.mod_micro_a * n_m
        # macroscopic absorption cross section of the moderator
        mod_macro_s = self.mod_micro_s * n_m
        # macroscopic scattering cross section of the moderator

        F = self.fuel_macro_a/(self.fuel_macro_a + mod_macro_a) # thermal utilization, F
    #dF/dTm
        d_f = -1*(self.fuel_macro_a * self.mod_micro_a * d_nm)/(
            (self.fuel_macro_a + mod_macro_a)**2)

        # Resonance escape integral, P
        P = math.exp((-1 * self.n_fuel * (self.fuel_volume) * self.I)/
                     ((mod_macro_s * 3000)))
        #dP/dTm
        d_p = P * (-1 * self.n_fuel * self.fuel_volume * unit.centi**3 *
                   (self.mod_micro_s) * d_nm)/(mod_macro_s * 3000 * unit.centi**3)**2

        e_th = 0.0862 * temp # convert temperature to energy in MeV
        e_one = mod_macro_s/math.log(self.E0/e_th)
        # neutron thermalization macroscopic cross section

        d_f = 1/(3 * mod_macro_s * (1 - self.mod_mu0)) # neutron diffusion coefficient
        tau = d_f/e_one # fermi age, tau
        #dTau/dTm
        d_tau = (((0.0862 * (e_th/self.E0)) * 3 * n_m) - math.log(self.E0/e_th) *
                 ((self.mod_micro_s * d_nm))/((3 * n_m)**2 * (1 - self.mod_mu0)))

        L = math.sqrt(1/(3 * mod_macro_s * mod_macro_a * (1 - self.mod_mu0)))
        # diffusion length L
        # dL/dTm
        d_l = 1/(2 * math.sqrt((-2 * d_nm * unit.zepto * unit.milli)/(3 * self.mod_micro_s * (self.mod_micro_a * (n_m * unit.zepto * unit.milli)**3 * ((1 - self.mod_mu0))))))

        # left term of the numerator of the moderator temperature feedback coefficient, alpha
        left_first_term = d_tau * (self.buckling**2 + L**2 * self.buckling**4)
        #holding L as constant
        left_second_term = d_l * (2 * L * self.buckling**2 + 2 * L *
                                  (tau * self.buckling**4)) # holding tau as constant
        left_term = (P * F) * (left_first_term + left_second_term)
        # combining with P and F held as constant

        right_1st_term = (-1) * (1 + ((tau + d_l**2) * self.buckling**2) + \
                tau * d_l**2 * self.buckling**4) # num as const

        right_first_term = (-1) * ((1 + ((tau + L**2) * self.buckling**2))
                                   + tau * L**2 * self.buckling**4) # num as const
        right_second_term = F * d_p # holding thermal utilization as constant
        right_third_term = P * d_f # holding resonance escpae as constant
        right_term = right_first_term * (right_second_term + right_third_term)
        # combining all three terms together

        # numerator and denominator
        numerator = left_term + right_term
        denominator = self.eta * self.epsilon * \
                (F * P)**2

        alpha_tn = numerator/denominator


        alpha_tn = alpha_tn/3

        return alpha_tn
示例#8
0
    def __get_coolant_outflow(self, time):
        """Get the coolant outflow stream.

        Parameters
        ----------
        time: float
            Time in SI unit.

        Returns
        -------
        None

        """

        coolant_outflow_stream = dict()

        outflow_cool_temp = self.coolant_outflow_phase.get_value('temp', time)

        if outflow_cool_temp <= 373.15:
            coolant_outflow_stream['temp'] = outflow_cool_temp
            coolant_outflow_stream['pressure'] = 0
            coolant_outflow_stream['quality'] = 0
            coolant_outflow_stream['flowrate'] = 0

        else:

            if self.params['valve_opened']:
                pressure = steam._PSat_T(outflow_cool_temp)
                base_temp = 373.15
                base_pressure = steam._PSat_T(base_temp)
                base_params = steam.IAPWS97(T=base_temp, x=0)
                base_entropy = base_params.s
                base_cp = base_params.cp
                inlet_params = steam.IAPWS97(T=outflow_cool_temp, x=0)
                inlet_cp = inlet_params.cp
                average_cp = (base_cp + inlet_cp)/2

                delta_s = average_cp * math.log(outflow_cool_temp/base_temp) - (unit.R/1000) * math.log(pressure/base_pressure)

                inlet_entropy = (delta_s + base_entropy) * 1.25
                bubl_entropy = inlet_params.s
                bubl_enthalpy = inlet_params.h

                inlet_params = steam.IAPWS97(T=base_temp, x=1)
                dew_entropy = inlet_params.s
                dew_enthalpy = inlet_params.h
                quality = (inlet_entropy - bubl_entropy)/(dew_entropy - bubl_entropy)

                delta_t = time - self.params['valve_opening_time']
                mass_flowrate = 1820 * (1 - math.exp(-1 * delta_t/(3 * unit.minute)))

                coolant_outflow_stream['temp'] = outflow_cool_temp
                coolant_outflow_stream['pressure'] = pressure
                coolant_outflow_stream['quality'] = quality
                coolant_outflow_stream['flowrate'] = mass_flowrate

            else:
                self.params['valve_opened'] = True
                self.params['valve_opening_time'] = time
                coolant_outflow_stream['temp'] = 373.15
                coolant_outflow_stream['pressure'] = 0
                coolant_outflow_stream['quality'] = 0
                coolant_outflow_stream['flowrate'] = 0

        return coolant_outflow_stream