A simple version of pure CO2. More...
#include <dumux/material/components/simpleco2.hh>
| Scalar | The type used for scalar values | 
| Public Types | |
| using | Scalar | 
| export the scalar type used by the component | |
| Static Public Member Functions | |
| static std::string | name () | 
| A human readable name for the CO2. | |
| static constexpr Scalar | molarMass () | 
| The mass in \(\mathrm{[kg/mol]}\) of one mole of CO2. | |
| static Scalar | criticalTemperature () | 
| Returns the critical temperature \(\mathrm{[K]}\) of CO2. | |
| static Scalar | criticalPressure () | 
| Returns the critical pressure \(\mathrm{[Pa]}\) of CO2. | |
| static Scalar | tripleTemperature () | 
| Returns the temperature \(\mathrm{[K]}\) at CO2's triple point. | |
| static Scalar | triplePressure () | 
| Returns the pressure \(\mathrm{[Pa]}\) at CO2's triple point. | |
| static const Scalar | gasEnthalpy (Scalar temperature, Scalar pressure) | 
| Specific enthalpy of CO2 \(\mathrm{[J/kg]}\). Shomate Equation is used for a temperature range of 298K to 6000K. | |
| static const Scalar | gasInternalEnergy (Scalar temperature, Scalar pressure) | 
| Specific internal energy of CO2 \(\mathrm{[J/kg]}\). | |
| static constexpr bool | gasIsCompressible () | 
| Returns true if the gas phase is assumed to be compressible. | |
| static constexpr bool | gasViscosityIsConstant () | 
| Returns true if the gas phase viscostiy is constant. | |
| static Scalar | gasDensity (Scalar temperature, Scalar pressure) | 
| The density \(\mathrm{[kg/m^3]}\) of CO2 at a given pressure and temperature. | |
| static Scalar | gasMolarDensity (Scalar temperature, Scalar pressure) | 
| The molar density of CO2 in \(\mathrm{[mol/m^3]}\) at a given pressure and temperature. | |
| static constexpr bool | gasIsIdeal () | 
| Returns true if the gas phase is assumed to be ideal. | |
| static Scalar | gasPressure (Scalar temperature, Scalar density) | 
| The pressure of CO2 in \(\mathrm{[Pa]}\) at a given density and temperature. | |
| static Scalar | gasViscosity (Scalar temperature, Scalar pressure) | 
| The dynamic viscosity \(\mathrm{[Pa*s]}\) of CO2. Equations given in: - Vesovic et al., 1990. | |
| static Scalar | gasThermalConductivity (Scalar temperature, Scalar pressure) | 
| Thermal conductivity \(\mathrm{[[W/(m*K)]}\) of CO2. | |
| static Scalar | gasHeatCapacity (Scalar temperature, Scalar pressure) | 
| Specific isobaric heat capacity of CO2 \(\mathrm{[J/(kg*K)]}\). Shomate Equation is used for a temperature range of 298K to 6000K. | |
| static void | init (Scalar tempMin, Scalar tempMax, unsigned nTemp, Scalar pressMin, Scalar pressMax, unsigned nPress) | 
| A default routine for initialization, not needed for components and must not be called. | |
| static Scalar | vaporPressure (Scalar t) | 
| The vapor pressure in \(\mathrm{[Pa]}\) of the component at a given temperature in \(\mathrm{[K]}\). | |
| Static Public Attributes | |
| static const ShomateMethod | shomateMethod | 
| static constexpr bool | isTabulated | 
| if the component relies on tabulated values | |
| 
 | inherited | 
| 
 | inlinestatic | 
| 
 | inlinestatic | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestatic | 
  Definition of enthalpy: \f$h= u + pv = u + p / \rho\f$.
  Rearranging for internal energy yields: \f$u = h - pv\f$.
  Exploiting the Ideal Gas assumption (\f$pv = R_{\textnormal{specific}} T\f$)gives: \f$u = h - R / M T \f$.
  The universal gas constant can only be used in the case of molar formulations.
 | temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| density | density of component in \(\mathrm{[kg/m^3]}\) | 
| 
 | inlinestatic | 
Thermal conductivity of CO2 at T=20°C, see: http://www.engineeringtoolbox.com/carbon-dioxide-d_1000.html
| temperature | absolute temperature in \(\mathrm{[K]}\) | 
| pressure | of the phase in \(\mathrm{[Pa]}\) | 
| 
 | inlinestatic | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) TODO: this does not look like a really "simple" parameterization. Can this be simplified further? | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticinherited | 
| tempMin | The minimum of the temperature range in \(\mathrm{[K]}\) | 
| tempMax | The maximum of the temperature range in \(\mathrm{[K]}\) | 
| nTemp | The number of entries/steps within the temperature range | 
| pressMin | The minimum of the pressure range in \(\mathrm{[Pa]}\) | 
| pressMax | The maximum of the pressure range in \(\mathrm{[Pa]}\) | 
| nPress | The number of entries/steps within the pressure range | 
This function throws a warning when called: "No init routine defined - make sure that this is not necessary!"
| 
 | inlinestaticconstexpr | 
| 
 | inlinestatic | 
| 
 | inlinestatic | 
| 
 | inlinestatic | 
| 
 | inlinestaticinherited | 
| t | temperature of the component in \(\mathrm{[K]}\) | 
| 
 | staticconstexprinherited | 
| 
 | static |