Properties of pure molecular oxygen \(O_2\). More...
#include <dumux/material/components/o2.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 \(O_2\). | |
| static constexpr Scalar | molarMass () | 
| The molar mass in \(\mathrm{[kg/mol]}\) of molecular oxygen. | |
| static constexpr Scalar | criticalTemperature () | 
| Returns the critical temperature in \(\mathrm{[K]}\) of molecular oxygen. | |
| static constexpr Scalar | criticalPressure () | 
| Returns the critical pressure in \(\mathrm{[Pa]}\) of molecular oxygen. | |
| static constexpr Scalar | tripleTemperature () | 
| Returns the temperature in \(\mathrm{[K]}\) at molecular oxygen's triple point. | |
| static constexpr Scalar | triplePressure () | 
| Returns the pressure in \(\mathrm{[Pa]}\) at molecular oxygen's triple point. | |
| static Scalar | vaporPressure (Scalar T) | 
| The vapor pressure in \(\mathrm{[Pa]}\) of pure molecular oxygen at a given temperature. | |
| static constexpr bool | gasIsCompressible () | 
| Returns true if the gas phase is assumed to be compressible. | |
| static constexpr Scalar | gasDensity (Scalar temperature, Scalar pressure) | 
| The density in \(\mathrm{[kg/m^3]}\) of pure \(O_2\) at a given pressure and temperature. | |
| static Scalar | gasMolarDensity (Scalar temperature, Scalar pressure) | 
| The molar density of pure \(O_2\) in \(\mathrm{[mol/m^3]}\), depending on pressure and temperature. | |
| static constexpr bool | gasIsIdeal () | 
| Returns true if the gas phase is assumed to be ideal. | |
| static constexpr Scalar | gasPressure (Scalar temperature, Scalar density) | 
| The pressure of gaseous \(O_2\) in \(\mathrm{[Pa]}\) at a given density and temperature. | |
| static Scalar | gasEnthalpy (Scalar temperature, Scalar pressure) | 
| Specific enthalpy \(\mathrm{[J/kg]}\) of pure oxygen gas. Shomate Equation is used for a temperature range of 100K to 6000K. | |
| static Scalar | gasHeatCapacity (Scalar T, Scalar pressure) | 
| Specific isobaric heat capacity \(\mathrm{[J/(kg*K)]}\) of pure oxygen gas. Shomate Equation is used for a temperature range of 100K to 6000K. | |
| static Scalar | gasViscosity (Scalar temperature, Scalar pressure) | 
| The dynamic viscosity \(\mathrm{[Pa*s]}\) of \(O_2\) at a given pressure and temperature. | |
| static constexpr Scalar | gasThermalConductivity (Scalar temperature, Scalar pressure) | 
| Thermal conductivity \(\mathrm{[[W/(m*K)]}\) of nitrogen. | |
| 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 constexpr bool | gasViscosityIsConstant () | 
| Returns true if the gas phase viscostiy is constant. | |
| static const Scalar | gasInternalEnergy (Scalar temperature, Scalar pressure) | 
| Specific internal energy \(\mathrm{[J/kg]}\) of the pure component in gas. | |
| Static Public Attributes | |
| static const ShomateMethod | shomateMethod | 
| static constexpr bool | isTabulated | 
| if the component relies on tabulated values | |
| 
 | inherited | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticconstexpr | 
| 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 | 
| T | absolute temperature in \(\mathrm{[K]}\) | 
| pressure | of the phase in \(\mathrm{[Pa]}\) | 
See: R. Reid, et al. (1987, pp 154, 657, 665) [reid1987]
| 
 | inlinestaticinherited | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| pressure | pressure of component in \(\mathrm{[Pa]}\) | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestatic | 
| temperature | The temperature of the gas | 
| pressure | The pressure of the gas | 
| 
 | inlinestaticconstexpr | 
| temperature | temperature of component in \(\mathrm{[K]}\) | 
| density | density of component in \(\mathrm{[kg/m^3]}\) | 
| 
 | inlinestaticconstexpr | 
Isobaric Properties for Nitrogen and Oxygen in: NIST Standard Reference Database Number 69, Eds. P.J. Linstrom and W.G. Mallard evaluated at p=.1 MPa, does not change dramatically with p and can be interpolated linearly with temperature
| 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 \(\mathrm{[Pa]}\) | 
See:
See: R. Reid, et al. (1987, pp 396-397, 664) [reid1987]
| 
 | inlinestaticconstexprinherited | 
| 
 | 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 | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestaticconstexpr | 
| 
 | inlinestatic | 
| T | temperature of component in \(\mathrm{[K]}\) | 
Taken from:
R. Prydz (1972, pp. 1-4) [prydz1972]
| 
 | staticconstexprinherited | 
| 
 | static |