3.4
DUNE for Multi-{Phase, Component, Scale, Physics, ...} flow and transport in porous media
air.hh
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24#ifndef DUMUX_AIR_HH
25#define DUMUX_AIR_HH
26
27#include <dune/common/math.hh>
28
33
34namespace Dumux {
35namespace Components {
36
43template <class Scalar>
44class Air
45: public Components::Base<Scalar, Air<Scalar> >
46, public Components::Gas<Scalar, Air<Scalar> >
47{
49
50public:
54 static std::string name()
55 { return "Air"; }
56
62 static constexpr Scalar molarMass()
63 { return 0.02896; /* [kg/mol] */ }
64
69 { return 132.6312; /* [K] */ }
70
75 { return 37.86e5; /* [Pa] */ }
76
86 {
87 // Assume an ideal gas
89 }
90
99
103 static constexpr bool gasIsCompressible()
104 { return true; }
105
109 static constexpr bool gasIsIdeal()
110 { return true; }
111
121 {
122 // Assume an ideal gas
124 }
125
150 {
151 const Scalar Tc = criticalTemperature();
152 const Scalar Vc = 84.525138; // critical specific volume [cm^3/mol]
153 const Scalar omega = 0.078; // accentric factor
154 const Scalar M = molarMass() * 1e3; // molar mas [g/mol]
155
156 const Scalar Fc = 1.0 - 0.2756*omega;
157 const Scalar Tstar = 1.2593*temperature/Tc;
158
159 using std::exp;
160 using std::pow;
161 const Scalar Omega_v = 1.16145*pow(Tstar, -0.14874)
162 + 0.52487*exp(-0.77320*Tstar)
163 + 2.16178*exp(-2.43787*Tstar);
164
165 using std::cbrt;
166 using std::sqrt;
167 const Scalar mu = 40.785 * Fc * sqrt(M * temperature)/(cbrt(Vc * Vc) * Omega_v);
168
169 // convertion from micro poise to Pa s
170 return mu/1.0e6/10.0;
171 }
172
188 {
189 // above 1200 K, the function becomes inaccurate
190 // since this should realistically never happen, we can live with it
191 const Scalar tempCelsius = temperature - 273.15;
192 const Scalar pressureCorrectionFactor = 9.7115e-9*tempCelsius*tempCelsius - 5.5e-6*tempCelsius + 0.0010809;
193
194 using std::sqrt;
195 const Scalar mu = 1.496e-6 * sqrt(temperature * temperature * temperature) / (temperature + 120.0)
196 * (1.0 + (pressure/1.0e5 - 1.0)*pressureCorrectionFactor);
197 return mu;
198 }
199
212 {
213 // above 1200 K, the function becomes inaccurate
214 // since this should realistically never happen, we can live with it
215 using std::sqrt;
216 return 1.496e-6 * sqrt(temperature * temperature * temperature) / (temperature + 120.0);
217 }
218
231 {
232 const Scalar epsk = 103.3; // [K]
233
234 using std::log;
235 using std::exp;
236 using std::sqrt;
237 const Scalar logTstar = log(temperature/epsk);
238 const Scalar Omega = exp(0.431
239 - 0.4623*logTstar
240 + 0.08406*logTstar*logTstar
241 + 0.005341*logTstar*logTstar*logTstar
242 - 0.00331*logTstar*logTstar*logTstar*logTstar);
243
244 const Scalar sigma = 0.36; // [nm]
245 const Scalar eta0 = 0.0266958*sqrt(1000.0*molarMass()*temperature)/(sigma*sigma*Omega);
246
247 using std::pow;
248 using Dune::power;
250 const Scalar rhoc = 10.4477; // [mol/m^3]
251 const Scalar delta = 0.001*pressure/(temperature*8.3144598)/rhoc;
252 const Scalar etaR = 10.72 * pow(tau, 0.2) * delta
253 + 1.122 * pow(tau, 0.05) * power(delta, 4)
254 + 0.002019 * pow(tau, 2.4) * power(delta, 9)
255 - 8.876 * pow(tau, 0.6) * delta * exp(-delta)
256 - 0.02916 * pow(tau, 3.6) * power(delta, 8) * exp(-delta);
257
258 return (eta0 + etaR)*1e-6;
259 }
260
271 {
273 }
274
288 {
290 - IdealGas::R * temperature // = pressure * molar volume for an ideal gas
291 / molarMass(); // conversion from [J/(mol K)] to [J/(kg K)]
292 }
293
309 {
310 // scale temperature with reference temp of 100K
311 Scalar phi = temperature/100;
312
313 using std::pow;
314 using Dune::power;
315 Scalar c_p = 0.661738E+01
316 -0.105885E+01 * phi
317 +0.201650E+00 * power(phi,2)
318 -0.196930E-01 * power(phi,3)
319 +0.106460E-02 * power(phi,4)
320 -0.303284E-04 * power(phi,5)
321 +0.355861E-06 * power(phi,6);
322 c_p += -0.549169E+01 * power(phi,-1)
323 +0.585171E+01 * power(phi,-2)
324 -0.372865E+01 * power(phi,-3)
325 +0.133981E+01 * power(phi,-4)
326 -0.233758E+00 * power(phi,-5)
327 +0.125718E-01 * power(phi,-6);
328 c_p *= IdealGas::R / molarMass(); // in J/(mol*K) / (kg/mol)
329
330 return c_p;
331 }
332
346 {
347 return 0.0255535;
348 }
349};
350
351} // end namespace Components
352} // end namespace Dumux
353
354#endif
Some exceptions thrown in DuMux
Interface for components that have a gas state.
Relations valid for an ideal gas.
Definition: adapt.hh:29
std::string temperature() noexcept
I/O name of temperature for equilibrium models.
Definition: name.hh:51
std::string pressure(int phaseIdx) noexcept
I/O name of pressure for multiphase systems.
Definition: name.hh:34
std::string density(int phaseIdx) noexcept
I/O name of density for multiphase systems.
Definition: name.hh:65
A class for the air fluid properties.
Definition: air.hh:47
static Scalar exactGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:230
static Scalar gasDensity(Scalar temperature, Scalar pressure)
The density of Air at a given pressure and temperature.
Definition: air.hh:85
static constexpr Scalar molarMass()
The molar mass in of Air.
Definition: air.hh:62
static const Scalar gasHeatCapacity(Scalar temperature, Scalar pressure)
Specific isobaric heat capacity of pure air.
Definition: air.hh:307
static Scalar criticalPressure()
Returns the critical pressure of Air.
Definition: air.hh:74
static Scalar gasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:187
static constexpr bool gasIsCompressible()
Returns true, the gas phase is assumed to be compressible.
Definition: air.hh:103
static Scalar gasThermalConductivity(Scalar temperature, Scalar pressure)
Thermal conductivity of air.
Definition: air.hh:345
static constexpr bool gasIsIdeal()
Returns true, the gas phase is assumed to be ideal.
Definition: air.hh:109
static Scalar simpleGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:211
static Scalar gasEnthalpy(Scalar temperature, Scalar pressure)
Specific enthalpy of Air with 273.15 as basis.
Definition: air.hh:270
static Scalar criticalTemperature()
Returns the critical temperature of Air.
Definition: air.hh:68
static Scalar oldGasViscosity(Scalar temperature, Scalar pressure)
The dynamic viscosity of Air at a given pressure and temperature.
Definition: air.hh:149
static const Scalar gasInternalEnergy(Scalar temperature, Scalar pressure)
Specific internal energy of Air .
Definition: air.hh:286
static std::string name()
A human readable name for Air.
Definition: air.hh:54
static Scalar gasPressure(Scalar temperature, Scalar density)
The pressure of gaseous Air at a given density and temperature.
Definition: air.hh:120
static Scalar gasMolarDensity(Scalar temperature, Scalar pressure)
The molar density of air in , depending on pressure and temperature.
Definition: air.hh:97
Base class for all components Components provide the thermodynamic relations for the liquid,...
Definition: components/base.hh:59
Scalar Scalar
export the scalar type used by the component
Definition: components/base.hh:63
Interface for components that have a gas state.
Definition: gas.hh:41
Relations valid for an ideal gas.
Definition: idealgas.hh:37
static constexpr Scalar pressure(Scalar temperature, Scalar rhoMolar)
The pressure of the gas in , depending on the molar density and temperature.
Definition: idealgas.hh:60
static constexpr Scalar R
The ideal gas constant .
Definition: idealgas.hh:40
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:49
static constexpr Scalar molarDensity(Scalar temperature, Scalar pressure)
The molar density of the gas , depending on pressure and temperature.
Definition: idealgas.hh:70
Base class for all components Components provide the thermodynamic relations for the liquid,...