version 3.8
air.hh
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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//
12#ifndef DUMUX_AIR_HH
13#define DUMUX_AIR_HH
14
15#include <dune/common/math.hh>
16
21
22namespace Dumux {
23namespace Components {
24
31template <class Scalar>
32class Air
33: public Components::Base<Scalar, Air<Scalar> >
34, public Components::Gas<Scalar, Air<Scalar> >
35{
37
38public:
42 static std::string name()
43 { return "Air"; }
44
50 static constexpr Scalar molarMass()
51 { return 0.02896; /* [kg/mol] */ }
52
57 { return 132.6312; /* [K] */ }
58
63 { return 37.86e5; /* [Pa] */ }
64
74 {
75 // Assume an ideal gas
77 }
78
87
91 static constexpr bool gasIsCompressible()
92 { return true; }
93
97 static constexpr bool gasIsIdeal()
98 { return true; }
99
103 static constexpr bool gasViscosityIsConstant()
104 { return false; }
105
115 {
116 // Assume an ideal gas
118 }
119
144 {
145 const Scalar Tc = criticalTemperature();
146 const Scalar Vc = 84.525138; // critical specific volume [cm^3/mol]
147 const Scalar omega = 0.078; // accentric factor
148 const Scalar M = molarMass() * 1e3; // molar mas [g/mol]
149
150 const Scalar Fc = 1.0 - 0.2756*omega;
151 const Scalar Tstar = 1.2593*temperature/Tc;
152
153 using std::exp;
154 using std::pow;
155 const Scalar Omega_v = 1.16145*pow(Tstar, -0.14874)
156 + 0.52487*exp(-0.77320*Tstar)
157 + 2.16178*exp(-2.43787*Tstar);
158
159 using std::cbrt;
160 using std::sqrt;
161 const Scalar mu = 40.785 * Fc * sqrt(M * temperature)/(cbrt(Vc * Vc) * Omega_v);
162
163 // conversion from micro poise to Pa s
164 return mu/1.0e6/10.0;
165 }
166
182 {
183 // above 1200 K, the function becomes inaccurate
184 // since this should realistically never happen, we can live with it
185 const Scalar tempCelsius = temperature - 273.15;
186 const Scalar pressureCorrectionFactor = 9.7115e-9*tempCelsius*tempCelsius - 5.5e-6*tempCelsius + 0.0010809;
187
188 using std::sqrt;
189 const Scalar mu = 1.496e-6 * sqrt(temperature * temperature * temperature) / (temperature + 120.0)
190 * (1.0 + (pressure/1.0e5 - 1.0)*pressureCorrectionFactor);
191 return mu;
192 }
193
206 {
207 // above 1200 K, the function becomes inaccurate
208 // since this should realistically never happen, we can live with it
209 using std::sqrt;
210 return 1.496e-6 * sqrt(temperature * temperature * temperature) / (temperature + 120.0);
211 }
212
225 {
226 const Scalar epsk = 103.3; // [K]
227
228 using std::log;
229 using std::exp;
230 using std::sqrt;
231 const Scalar logTstar = log(temperature/epsk);
232 const Scalar Omega = exp(0.431
233 - 0.4623*logTstar
234 + 0.08406*logTstar*logTstar
235 + 0.005341*logTstar*logTstar*logTstar
236 - 0.00331*logTstar*logTstar*logTstar*logTstar);
237
238 const Scalar sigma = 0.36; // [nm]
239 const Scalar eta0 = 0.0266958*sqrt(1000.0*molarMass()*temperature)/(sigma*sigma*Omega);
240
241 using std::pow;
242 using Dune::power;
244 const Scalar rhoc = 10.4477; // [mol/m^3]
245 const Scalar delta = 0.001*pressure/(temperature*8.3144598)/rhoc;
246 const Scalar etaR = 10.72 * pow(tau, 0.2) * delta
247 + 1.122 * pow(tau, 0.05) * power(delta, 4)
248 + 0.002019 * pow(tau, 2.4) * power(delta, 9)
249 - 8.876 * pow(tau, 0.6) * delta * exp(-delta)
250 - 0.02916 * pow(tau, 3.6) * power(delta, 8) * exp(-delta);
251
252 return (eta0 + etaR)*1e-6;
253 }
254
265 {
267 }
268
282 {
284 - IdealGas::R * temperature // = pressure * molar volume for an ideal gas
285 / molarMass(); // conversion from [J/(mol K)] to [J/(kg K)]
286 }
287
303 {
304 // scale temperature with reference temp of 100K
305 Scalar phi = temperature/100;
306
307 using std::pow;
308 using Dune::power;
309 Scalar c_p = 0.661738E+01
310 -0.105885E+01 * phi
311 +0.201650E+00 * power(phi,2)
312 -0.196930E-01 * power(phi,3)
313 +0.106460E-02 * power(phi,4)
314 -0.303284E-04 * power(phi,5)
315 +0.355861E-06 * power(phi,6);
316 c_p += -0.549169E+01 * power(phi,-1)
317 +0.585171E+01 * power(phi,-2)
318 -0.372865E+01 * power(phi,-3)
319 +0.133981E+01 * power(phi,-4)
320 -0.233758E+00 * power(phi,-5)
321 +0.125718E-01 * power(phi,-6);
322 c_p *= IdealGas::R / molarMass(); // in J/(mol*K) / (kg/mol)
323
324 return c_p;
325 }
326
340 {
341 return 0.0255535;
342 }
343};
344
345} // end namespace Components
346} // end namespace Dumux
347
348#endif
A class for the air fluid properties.
Definition: air.hh:35
static Scalar exactGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:224
static Scalar gasDensity(Scalar temperature, Scalar pressure)
The density of Air at a given pressure and temperature.
Definition: air.hh:73
static constexpr Scalar molarMass()
The molar mass in of Air.
Definition: air.hh:50
static const Scalar gasHeatCapacity(Scalar temperature, Scalar pressure)
Specific isobaric heat capacity of pure air.
Definition: air.hh:301
static Scalar criticalPressure()
Returns the critical pressure of Air.
Definition: air.hh:62
static Scalar gasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:181
static constexpr bool gasIsCompressible()
Returns true, the gas phase is assumed to be compressible.
Definition: air.hh:91
static Scalar gasThermalConductivity(Scalar temperature, Scalar pressure)
Thermal conductivity of air.
Definition: air.hh:339
static constexpr bool gasViscosityIsConstant()
Returns true if the gas phase viscosity is constant.
Definition: air.hh:103
static constexpr bool gasIsIdeal()
Returns true, the gas phase is assumed to be ideal.
Definition: air.hh:97
static Scalar simpleGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:205
static Scalar gasEnthalpy(Scalar temperature, Scalar pressure)
Specific enthalpy of Air with 273.15 as basis.
Definition: air.hh:264
static Scalar criticalTemperature()
Returns the critical temperature of Air.
Definition: air.hh:56
static Scalar oldGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:143
static const Scalar gasInternalEnergy(Scalar temperature, Scalar pressure)
Specific internal energy of Air .
Definition: air.hh:280
static std::string name()
A human readable name for Air.
Definition: air.hh:42
static Scalar gasPressure(Scalar temperature, Scalar density)
The pressure of gaseous Air at a given density and temperature.
Definition: air.hh:114
static Scalar gasMolarDensity(Scalar temperature, Scalar pressure)
The molar density of air in , depending on pressure and temperature.
Definition: air.hh:85
Base class for all components Components provide the thermodynamic relations for the liquid,...
Definition: components/base.hh:47
Scalar Scalar
export the scalar type used by the component
Definition: components/base.hh:51
Interface for components that have a gas state.
Definition: gas.hh:29
Relations valid for an ideal gas.
Definition: idealgas.hh:25
static constexpr Scalar pressure(Scalar temperature, Scalar rhoMolar)
The pressure of the gas in , depending on the molar density and temperature.
Definition: idealgas.hh:48
static constexpr Scalar R
The ideal gas constant .
Definition: idealgas.hh:28
static constexpr Scalar density(Scalar avgMolarMass, Scalar temperature, Scalar pressure)
The density of the gas in , depending on pressure, temperature and average molar mass of the gas.
Definition: idealgas.hh:37
static constexpr Scalar molarDensity(Scalar temperature, Scalar pressure)
The molar density of the gas , depending on pressure and temperature.
Definition: idealgas.hh:58
Base class for all components Components provide the thermodynamic relations for the liquid,...
Some exceptions thrown in DuMux
Interface for components that have a gas state.
Relations valid for an ideal gas.
std::string temperature() noexcept
I/O name of temperature for equilibrium models.
Definition: name.hh:39
std::string pressure(int phaseIdx) noexcept
I/O name of pressure for multiphase systems.
Definition: name.hh:22
std::string density(int phaseIdx) noexcept
I/O name of density for multiphase systems.
Definition: name.hh:53
Definition: adapt.hh:17