diff --git a/dumux/material/components/air.hh b/dumux/material/components/air.hh index 1a5c751808020236d91ff600790e8f56247499e8..dbf908fe395d3ba75d98a3a8b5c81c70653bb16b 100644 --- a/dumux/material/components/air.hh +++ b/dumux/material/components/air.hh @@ -46,13 +46,13 @@ class Air : public Component > public: /*! - * \brief A human readable name for the \f$Air\f$. + * \brief A human readable name for Air. */ static const char *name() { return "Air"; } /*! - * \brief The molar mass in \f$\mathrm{[kg/mol]}\f$ of \f$AIR\f$. + * \brief The molar mass in \f$\mathrm{[kg/mol]}\f$ of Air. * * Taken from constrelair.hh. */ @@ -60,19 +60,21 @@ public: { return 0.02896; /* [kg/mol] */ } /*! - * \brief Returns the critical temperature \f$\mathrm{[K]}\f$ of \f$AIR\f$. + * \brief Returns the critical temperature \f$\mathrm{[K]}\f$ of Air. */ static Scalar criticalTemperature() { return 132.531 ; /* [K] */ } /*! - * \brief Returns the critical pressure \f$\mathrm{[Pa]}\f$ of \f$AIR\f$. + * \brief Returns the critical pressure \f$\mathrm{[Pa]}\f$ of Air. */ static Scalar criticalPressure() { return 37.86e5; /* [Pa] */ } /*! - * \brief The density of \f$AIR\f$ at a given pressure and temperature \f$\mathrm{[kg/m^3]}\f$. + * \brief The density \f$\mathrm{[kg/m^3]}\f$ of Air at a given pressure and temperature. + * + * Ideal gas is assumed. * * \param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param pressure pressure of phase in \f$\mathrm{[Pa]}\f$ @@ -84,19 +86,21 @@ public: } /*! - * \brief Returns true iff the gas phase is assumed to be compressible + * \brief Returns true, the gas phase is assumed to be compressible */ static bool gasIsCompressible() { return true; } /*! - * \brief Returns true iff the gas phase is assumed to be ideal + * \brief Returns true, the gas phase is assumed to be ideal */ static bool gasIsIdeal() { return true; } /*! - * \brief The pressure of gaseous \f$AIR\f$ at a given density and temperature \f$\mathrm{[Pa]}\f$. + * \brief The pressure \f$\mathrm{[Pa]}\f$ of gaseous Air at a given density and temperature. + * + * Ideal gas is assumed. * * \param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param density density of component in \f$\mathrm{[kg/m^3]}\f$ @@ -107,18 +111,18 @@ public: return IdealGas::pressure(temperature, density/molarMass()); } /*! - * \brief The dynamic viscosity \f$\mathrm{[Pa*s]}\f$ of \f$AIR\f$ at a given pressure and temperature. Criticial specific - * volume calculated by \f$V_c = (R*T_c)/p_c\f$. + * \brief The dynamic viscosity \f$\mathrm{[Pa*s]}\f$ of Air at a given pressure and temperature. * - * \param temperature temperature of component in \f$\mathrm{[K]}\f$ - * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ + * Criticial specific volume calculated by \f$V_c = (R*T_c)/p_c\f$. * * Reid et al. (1987, pp 396-397, 667) \cite reid1987
* Poling et al. (2001, pp 9.7-9.8) \cite poling2001
* * Accentric factor taken from:
- * Adebiyi (2003) \cite adebiyi2003 + * Adebiyi (2003) \cite adebiyi2003 * + * \param temperature temperature of component in \f$\mathrm{[K]}\f$ + * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ */ static Scalar gasViscosity(Scalar temperature, Scalar pressure) { @@ -160,7 +164,7 @@ public: } /*! - * \brief Specific enthalpy of air \f$\mathrm{[J/kg]}\f$ + * \brief Specific enthalpy of Air \f$\mathrm{[J/kg]}\f$ * with 273.15 \f$K \f$ as basis.
* * \param temperature temperature of component in \f$\mathrm{[K]}\f$ @@ -174,7 +178,7 @@ public: } /*! - * \brief Specific internal energy of \f$AIR\f$ \f$\mathrm{[J/kg]}\f$. + * \brief Specific internal energy of Air \f$\mathrm{[J/kg]}\f$. * * Definition of enthalpy: \f$h= u + pv = u + p / \rho\f$. * Rearranging for internal energy yields: \f$u = h - pv\f$.