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1 | // -*- mode: C++; tab-width: 4; indent-tabs-mode: nil; c-basic-offset: 4 -*- | ||
2 | // vi: set et ts=4 sw=4 sts=4: | ||
3 | // | ||
4 | // SPDX-FileCopyrightInfo: Copyright © DuMux Project contributors, see AUTHORS.md in root folder | ||
5 | // SPDX-License-Identifier: GPL-3.0-or-later | ||
6 | // | ||
7 | /*! | ||
8 | * \file | ||
9 | * \ingroup Components | ||
10 | * \brief Properties of pure molecular oxygen \f$O_2\f$. | ||
11 | */ | ||
12 | #ifndef DUMUX_O2_HH | ||
13 | #define DUMUX_O2_HH | ||
14 | |||
15 | #include <dumux/material/idealgas.hh> | ||
16 | |||
17 | #include <cmath> | ||
18 | |||
19 | #include <dumux/material/components/base.hh> | ||
20 | #include <dumux/material/components/gas.hh> | ||
21 | |||
22 | namespace Dumux { | ||
23 | namespace Components { | ||
24 | |||
25 | /*! | ||
26 | * \ingroup Components | ||
27 | * \brief Properties of pure molecular oxygen \f$O_2\f$. | ||
28 | * | ||
29 | * \tparam Scalar The type used for scalar values | ||
30 | */ | ||
31 | template <class Scalar> | ||
32 | class O2 | ||
33 | : public Components::Base<Scalar, O2<Scalar> > | ||
34 | , public Components::Gas<Scalar, O2<Scalar> > | ||
35 | { | ||
36 | using IdealGas = Dumux::IdealGas<Scalar>; | ||
37 | |||
38 | public: | ||
39 | /*! | ||
40 | * \brief A human readable name for the \f$O_2\f$. | ||
41 | */ | ||
42 | static std::string name() | ||
43 |
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|
34 | { return "O2"; } |
44 | |||
45 | /*! | ||
46 | * \brief The molar mass in \f$\mathrm{[kg/mol]}\f$ of molecular oxygen. | ||
47 | */ | ||
48 | static constexpr Scalar molarMass() | ||
49 | { return 32e-3; } | ||
50 | |||
51 | /*! | ||
52 | * \brief Returns the critical temperature in \f$\mathrm{[K]}\f$ of molecular oxygen. | ||
53 | */ | ||
54 | static constexpr Scalar criticalTemperature() | ||
55 | { return 154.581; /* [K] */ } | ||
56 | |||
57 | /*! | ||
58 | * \brief Returns the critical pressure in \f$\mathrm{[Pa]}\f$ of molecular oxygen. | ||
59 | */ | ||
60 | static constexpr Scalar criticalPressure() | ||
61 | { return 5.0804e6; /* [N/m^2] */ } | ||
62 | |||
63 | /*! | ||
64 | * \brief Returns the temperature in \f$\mathrm{[K]}\f$ at molecular oxygen's triple point. | ||
65 | */ | ||
66 | static constexpr Scalar tripleTemperature() | ||
67 | { return 54.359; /* [K] */ } | ||
68 | |||
69 | /*! | ||
70 | * \brief Returns the pressure in \f$\mathrm{[Pa]}\f$ at molecular oxygen's triple point. | ||
71 | */ | ||
72 | static constexpr Scalar triplePressure() | ||
73 | { return 148.0; /* [N/m^2] */ } | ||
74 | |||
75 | /*! | ||
76 | * \brief The vapor pressure in \f$\mathrm{[Pa]}\f$ of pure molecular oxygen | ||
77 | * at a given temperature. | ||
78 | * | ||
79 | * \param T temperature of component in \f$\mathrm{[K]}\f$ | ||
80 | * | ||
81 | * Taken from: | ||
82 | * | ||
83 | * R. Prydz (1972, pp. 1-4) \cite prydz1972 | ||
84 | */ | ||
85 | 3 | static Scalar vaporPressure(Scalar T) | |
86 | { | ||
87 |
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3 | if (T > criticalTemperature()) |
88 | return criticalPressure(); | ||
89 | ✗ | if (T < tripleTemperature()) | |
90 | return 0; // O2 is solid: We don't take sublimation into account | ||
91 | |||
92 | // vapor pressure between tripe and critical points. See the | ||
93 | // paper of Prydz for a discussion | ||
94 | ✗ | Scalar X = | |
95 | ✗ | (1 - tripleTemperature()/T) / | |
96 | (1 - tripleTemperature()/criticalTemperature()); | ||
97 | ✗ | const Scalar A = 7.568956; | |
98 | ✗ | const Scalar B = 5.004836; | |
99 | ✗ | const Scalar C = -2.137460; | |
100 | ✗ | const Scalar D = 3.454481; | |
101 | ✗ | const Scalar epsilon = 1.514; | |
102 | |||
103 | using std::exp; | ||
104 | using std::pow; | ||
105 | ✗ | return triplePressure()*exp(X*(A + X*(B + C*X) + D*pow(1 - X, epsilon))); | |
106 | } | ||
107 | |||
108 | /*! | ||
109 | * \brief Returns true if the gas phase is assumed to be compressible | ||
110 | */ | ||
111 | static constexpr bool gasIsCompressible() | ||
112 | { return true; } | ||
113 | |||
114 | /*! | ||
115 | * \brief The density in \f$\mathrm{[kg/m^3]}\f$ of pure \f$O_2\f$ at a given pressure and temperature. | ||
116 | * | ||
117 | * \param temperature temperature of component in \f$\mathrm{[K]}\f$ | ||
118 | * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ | ||
119 | * | ||
120 | * \todo: density liquid oxygen | ||
121 | */ | ||
122 | static constexpr Scalar gasDensity(Scalar temperature, Scalar pressure) | ||
123 | { | ||
124 | // Assume an ideal gas | ||
125 |
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603656 | return IdealGas::density(molarMass(), temperature, pressure); |
126 | } | ||
127 | |||
128 | /*! | ||
129 | * \brief The molar density of pure \f$O_2\f$ in \f$\mathrm{[mol/m^3]}\f$, | ||
130 | * depending on pressure and temperature. | ||
131 | * \param temperature The temperature of the gas | ||
132 | * \param pressure The pressure of the gas | ||
133 | */ | ||
134 | static Scalar gasMolarDensity(Scalar temperature, Scalar pressure) | ||
135 | 603430 | { return IdealGas::molarDensity(temperature, pressure); } | |
136 | |||
137 | /*! | ||
138 | * \brief Returns true if the gas phase is assumed to be ideal | ||
139 | */ | ||
140 | static constexpr bool gasIsIdeal() | ||
141 | { return true; } | ||
142 | |||
143 | /*! | ||
144 | * \brief The pressure of gaseous \f$O_2\f$ in \f$\mathrm{[Pa]}\f$ at a given density and temperature. | ||
145 | * | ||
146 | * \param temperature temperature of component in \f$\mathrm{[K]}\f$ | ||
147 | * \param density density of component in \f$\mathrm{[kg/m^3]}\f$ | ||
148 | */ | ||
149 | static constexpr Scalar gasPressure(Scalar temperature, Scalar density) | ||
150 | { | ||
151 | // Assume an ideal gas | ||
152 | 18 | return IdealGas::pressure(temperature, density/molarMass()); | |
153 | } | ||
154 | |||
155 | /*! | ||
156 | * \brief Specific enthalpy \f$\mathrm{[J/kg]}\f$ of pure oxygen gas. | ||
157 | * | ||
158 | * \param temperature temperature of component in \f$\mathrm{[K]}\f$ | ||
159 | * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ | ||
160 | */ | ||
161 | ✗ | static Scalar gasEnthalpy(Scalar temperature, | |
162 | Scalar pressure) | ||
163 | { | ||
164 | 279034 | return gasHeatCapacity(temperature, pressure) * temperature; | |
165 | } | ||
166 | |||
167 | /*! | ||
168 | * \brief Specific isobaric heat capacity \f$\mathrm{[J/(kg*K)]}\f$ of pure | ||
169 | * oxygen gas. | ||
170 | * | ||
171 | * This is equivalent to the partial derivative of the specific | ||
172 | * enthalpy to the temperature. | ||
173 | * \param T absolute temperature in \f$\mathrm{[K]}\f$ | ||
174 | * \param pressure of the phase in \f$\mathrm{[Pa]}\f$ | ||
175 | * | ||
176 | * See: R. Reid, et al. (1987, pp 154, 657, 665) \cite reid1987 | ||
177 | */ | ||
178 | ✗ | static Scalar gasHeatCapacity(Scalar T, | |
179 | Scalar pressure) | ||
180 | { | ||
181 | // method of Joback | ||
182 | 139629 | const Scalar cpVapA = 28.11; | |
183 | 139629 | const Scalar cpVapB = -3.680e-6; | |
184 | 139629 | const Scalar cpVapC = 1.746e-5; | |
185 | 139629 | const Scalar cpVapD = -1.065e-8; | |
186 | |||
187 | return | ||
188 | 1/molarMass()* // conversion from [J/(mol*K)] to [J/(kg*K)] | ||
189 | 139629 | (cpVapA + T* | |
190 | 139629 | (cpVapB/2 + T* | |
191 | 139629 | (cpVapC/3 + T* | |
192 | 139629 | (cpVapD/4)))); | |
193 | } | ||
194 | |||
195 | /*! | ||
196 | * \brief The dynamic viscosity \f$\mathrm{[Pa*s]}\f$ of \f$O_2\f$ at a given pressure and temperature. | ||
197 | * | ||
198 | * \param temperature temperature of component in \f$\mathrm{[K]}\f$ | ||
199 | * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ | ||
200 | * | ||
201 | * See: | ||
202 | * | ||
203 | * See: R. Reid, et al. (1987, pp 396-397, 664) \cite reid1987 | ||
204 | */ | ||
205 | 301825 | static Scalar gasViscosity(Scalar temperature, Scalar pressure) | |
206 | { | ||
207 | 301825 | const Scalar Tc = criticalTemperature(); | |
208 | 301825 | const Scalar Vc = 73.4; // critical specific volume [cm^3/mol] | |
209 | 301825 | const Scalar omega = 0.025; // accentric factor | |
210 | 301825 | const Scalar M = molarMass() * 1e3; // molar mas [g/mol] | |
211 | 301825 | const Scalar dipole = 0.0; // dipole moment [debye] | |
212 | |||
213 | using std::sqrt; | ||
214 | 301825 | Scalar mu_r4 = 131.3 * dipole / sqrt(Vc * Tc); | |
215 | 301825 | mu_r4 *= mu_r4; | |
216 | 301825 | mu_r4 *= mu_r4; | |
217 | |||
218 | 301825 | Scalar Fc = 1 - 0.2756*omega + 0.059035*mu_r4; | |
219 | 301825 | Scalar Tstar = 1.2593 * temperature/Tc; | |
220 | |||
221 | using std::pow; | ||
222 | using std::exp; | ||
223 | 301825 | Scalar Omega_v = | |
224 | 603650 | 1.16145*pow(Tstar, -0.14874) + | |
225 | 301825 | 0.52487*exp(- 0.77320*Tstar) + | |
226 | 301825 | 2.16178*exp(- 2.43787*Tstar); | |
227 | 301825 | Scalar mu = 40.785*Fc*sqrt(M*temperature)/(pow(Vc, 2./3)*Omega_v); | |
228 | |||
229 | // conversion from micro poise to Pa s | ||
230 | 301825 | return mu/1e6 / 10; | |
231 | } | ||
232 | |||
233 | /*! | ||
234 | * \brief Thermal conductivity \f$\mathrm{[[W/(m*K)]}\f$ of nitrogen. | ||
235 | * | ||
236 | * Isobaric Properties for Nitrogen and Oxygen in: NIST Standard | ||
237 | * Reference Database Number 69, Eds. P.J. Linstrom and | ||
238 | * W.G. Mallard evaluated at p=.1 MPa, does not | ||
239 | * change dramatically with p and can be interpolated linearly with temperature | ||
240 | * | ||
241 | * \param temperature absolute temperature in \f$\mathrm{[K]}\f$ | ||
242 | * \param pressure of the phase in \f$\mathrm{[Pa]}\f$ | ||
243 | */ | ||
244 | ✗ | static constexpr Scalar gasThermalConductivity(Scalar temperature, Scalar pressure) | |
245 | { | ||
246 | 139517 | return 8.044e-5 * (temperature - 273.15) + 0.024486; | |
247 | } | ||
248 | }; | ||
249 | |||
250 | } // end namespace Components | ||
251 | |||
252 | } // end namespace Dumux | ||
253 | |||
254 | #endif | ||
255 |