Properties of pure molecular oxygen O_2. More...
#include <dumux/material/components/o2.hh>
Properties of pure molecular oxygen O_2.
Scalar | The type used for scalar values |
Public Types | |
using | Scalar = Scalar |
export the scalar type used by the component More... | |
Static Public Member Functions | |
static std::string | name () |
A human readable name for the O_2. More... | |
static constexpr Scalar | molarMass () |
The molar mass in \mathrm{[kg/mol]} of molecular oxygen. More... | |
static constexpr Scalar | criticalTemperature () |
Returns the critical temperature in \mathrm{[K]} of molecular oxygen. More... | |
static constexpr Scalar | criticalPressure () |
Returns the critical pressure in \mathrm{[Pa]} of molecular oxygen. More... | |
static constexpr Scalar | tripleTemperature () |
Returns the temperature in \mathrm{[K]} at molecular oxygen's triple point. More... | |
static constexpr Scalar | triplePressure () |
Returns the pressure in \mathrm{[Pa]} at molecular oxygen's triple point. More... | |
static Scalar | vaporPressure (Scalar T) |
The vapor pressure in \mathrm{[Pa]} of pure molecular oxygen at a given temperature. More... | |
static constexpr bool | gasIsCompressible () |
Returns true if the gas phase is assumed to be compressible. More... | |
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. More... | |
static Scalar | gasMolarDensity (Scalar temperature, Scalar pressure) |
The molar density of pure O_2 in \mathrm{[mol/m^3]}, depending on pressure and temperature. More... | |
static constexpr bool | gasIsIdeal () |
Returns true if the gas phase is assumed to be ideal. More... | |
static constexpr Scalar | gasPressure (Scalar temperature, Scalar density) |
The pressure of gaseous O_2 in \mathrm{[Pa]} at a given density and temperature. More... | |
static Scalar | gasEnthalpy (Scalar temperature, Scalar pressure) |
Specific enthalpy \mathrm{[J/kg]} of pure oxygen gas. More... | |
static Scalar | gasHeatCapacity (Scalar T, Scalar pressure) |
Specific isobaric heat capacity \mathrm{[J/(kg*K)]} of pure oxygen gas. More... | |
static Scalar | gasViscosity (Scalar temperature, Scalar pressure) |
The dynamic viscosity \mathrm{[Pa*s]} of O_2 at a given pressure and temperature. More... | |
static constexpr Scalar | gasThermalConductivity (Scalar temperature, Scalar pressure) |
Thermal conductivity \mathrm{[[W/(m*K)]} of nitrogen. More... | |
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. More... | |
static constexpr bool | gasViscosityIsConstant () |
Returns true if the gas phase viscostiy is constant. More... | |
static const Scalar | gasInternalEnergy (Scalar temperature, Scalar pressure) |
Specific internal energy \mathrm{[J/kg]} of the pure component in gas. More... | |
Static Public Attributes | |
static constexpr bool | isTabulated |
if the component relies on tabulated values More... | |
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inherited |
export the scalar type used by the component
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inlinestaticconstexpr |
Returns the critical pressure in \mathrm{[Pa]} of molecular oxygen.
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inlinestaticconstexpr |
Returns the critical temperature in \mathrm{[K]} of molecular oxygen.
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inlinestaticconstexpr |
The density in \mathrm{[kg/m^3]} of pure O_2 at a given pressure and temperature.
temperature | temperature of component in \mathrm{[K]} |
pressure | pressure of component in \mathrm{[Pa]} |
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inlinestatic |
Specific enthalpy \mathrm{[J/kg]} of pure oxygen gas.
temperature | temperature of component in \mathrm{[K]} |
pressure | pressure of component in \mathrm{[Pa]} |
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inlinestatic |
Specific isobaric heat capacity \mathrm{[J/(kg*K)]} of pure oxygen gas.
This is equivalent to the partial derivative of the specific enthalpy to the temperature.
T | absolute temperature in \mathrm{[K]} |
pressure | of the phase in \mathrm{[Pa]} |
See: R. Reid, et al. (1987, pp 154, 657, 665) [59]
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inlinestaticinherited |
Specific internal energy \mathrm{[J/kg]} of the pure component in gas.
temperature | temperature of component in \mathrm{[K]} |
pressure | pressure of component in \mathrm{[Pa]} |
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inlinestaticconstexpr |
Returns true if the gas phase is assumed to be compressible.
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inlinestaticconstexpr |
Returns true if the gas phase is assumed to be ideal.
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inlinestatic |
The molar density of pure O_2 in \mathrm{[mol/m^3]}, depending on pressure and temperature.
temperature | The temperature of the gas |
pressure | The pressure of the gas |
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inlinestaticconstexpr |
The pressure of gaseous O_2 in \mathrm{[Pa]} at a given density and temperature.
temperature | temperature of component in \mathrm{[K]} |
density | density of component in \mathrm{[kg/m^3]} |
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inlinestaticconstexpr |
Thermal conductivity \mathrm{[[W/(m*K)]} of nitrogen.
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]} |
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inlinestatic |
The dynamic viscosity \mathrm{[Pa*s]} of O_2 at a given pressure and temperature.
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) [59]
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inlinestaticconstexprinherited |
Returns true if the gas phase viscostiy is constant.
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inlinestaticinherited |
A default routine for initialization, not needed for components and must not be called.
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!"
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inlinestaticconstexpr |
The molar mass in \mathrm{[kg/mol]} of molecular oxygen.
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inlinestatic |
A human readable name for the O_2.
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inlinestaticconstexpr |
Returns the pressure in \mathrm{[Pa]} at molecular oxygen's triple point.
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inlinestaticconstexpr |
Returns the temperature in \mathrm{[K]} at molecular oxygen's triple point.
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inlinestatic |
The vapor pressure in \mathrm{[Pa]} of pure molecular oxygen at a given temperature.
T | temperature of component in \mathrm{[K]} |
Taken from:
R. Prydz (1972, pp. 1-4) [57]
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staticconstexprinherited |
if the component relies on tabulated values