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Commit 9702abcc authored by Kilian Weishaupt's avatar Kilian Weishaupt
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[doxygen] Add bibtex references

The handbook bibliography is now also used
for citing references via doxygen.
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...@@ -26,4 +26,6 @@ SERVER_BASED_SEARCH = NO ...@@ -26,4 +26,6 @@ SERVER_BASED_SEARCH = NO
# disable macro expansion (Otherwise, certain properties will not appear # disable macro expansion (Otherwise, certain properties will not appear
# in the documentation properly. This should be fixed at some time.) # in the documentation properly. This should be fixed at some time.)
MACRO_EXPANSION = NO MACRO_EXPANSION = NO
\ No newline at end of file
CITE_BIB_FILES = @top_srcdir@/doc/handbook/dumux-handbook
...@@ -77,6 +77,17 @@ ...@@ -77,6 +77,17 @@
pages = {in print} pages = {in print}
} }
@inproceedings{adebiyi2003,
title={Formulations for the thermodynamic properties of pure substances},
author={Adebiyi, George A},
booktitle={ASME 2003 International Mechanical Engineering Congress and Exposition},
pages={183--188},
year={2003},
organization={American Society of Mechanical Engineers},
url = {https://dx.doi.org/10.1115/IMECE2003-41299}
}
@ARTICLE{AGRAWAL2001, @ARTICLE{AGRAWAL2001,
author = {K. Agrawal and P. N. Loezos and M. Syamlal and S. Sundaresan}, author = {K. Agrawal and P. N. Loezos and M. Syamlal and S. Sundaresan},
title = {The Role of Meso-Scale Structures in Rapid Gas-Solid Flows}, title = {The Role of Meso-Scale Structures in Rapid Gas-Solid Flows},
...@@ -502,6 +513,14 @@ ...@@ -502,6 +513,14 @@
edition = {1} edition = {1}
} }
@article{hollis1996,
title={{Real-Gas Flow Properties for NASA Langley Research Center Aerothermodynamic Facilities Complex Wind Tunnels}},
author={BR, Hollis},
year={1996},
publisher={NASA Langley Technical Report Server}
}
@BOOK{HYDROSKRIPT, @BOOK{HYDROSKRIPT,
title = {Grundlagen der Hydromechanik}, title = {Grundlagen der Hydromechanik},
publisher = {Shaker}, publisher = {Shaker},
...@@ -562,6 +581,14 @@ ...@@ -562,6 +581,14 @@
edition = {1} edition = {1}
} }
@BOOK{kays2005,
title = {Convective heat and mass transfer},
publisher = {McGraw-Hill Higher Education},
year = {2005},
author = {W. M. Kays and M. E. Crawford and B. Weigand},
edition = {4},
}
@ARTICLE{A3:King:1996, @ARTICLE{A3:King:1996,
author = {King, P. R.}, author = {King, P. R.},
title = {Upscaling Permeability: Error Analysis for Renormalisation}, title = {Upscaling Permeability: Error Analysis for Renormalisation},
...@@ -795,6 +822,16 @@ ...@@ -795,6 +822,16 @@
author = {Reid, R.C. and Prausnitz, J.M. and Poling, B.E.} author = {Reid, R.C. and Prausnitz, J.M. and Poling, B.E.}
} }
@book{poling2001,
title={The properties of gases and liquids},
author={Poling, Bruce E and Prausnitz, John M and O'connell, John P and others},
volume={5},
year={2001},
publisher={McGraw-Hill New York}
}
@ARTICLE{Pardiso, @ARTICLE{Pardiso,
author = {Olaf Schenk and Klaus G\"artner}, author = {Olaf Schenk and Klaus G\"artner},
title = {Solving unsymmetric sparse systems of linear equations with {PARDISO}}, title = {Solving unsymmetric sparse systems of linear equations with {PARDISO}},
...@@ -1005,6 +1042,11 @@ ...@@ -1005,6 +1042,11 @@
key = {FENICS} key = {FENICS}
} }
@MISC{NIST,
title = {Thermophysical Properties of Fluid Systems: \url{http://webbook.nist.gov/chemistry/fluid/}},
key = {NIST}
}
@MISC{STL-REF-HP, @MISC{STL-REF-HP,
title = {A {STL} Reference: \url{http://www.cplusplus.com/reference/stl/}}, title = {A {STL} Reference: \url{http://www.cplusplus.com/reference/stl/}},
key = {STL} key = {STL}
......
...@@ -107,24 +107,17 @@ public: ...@@ -107,24 +107,17 @@ public:
return IdealGas::pressure(temperature, density/molarMass()); 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. * \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$V_c = (R*T_c)/p_c\f$.
* *
*\param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param temperature temperature of component in \f$\mathrm{[K]}\f$
* \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$
* *
* See: * Reid et al. (1987, pp 396-397, 667) \cite reid1987 <BR>
* * Poling et al. (2001, pp 9.7-9.8) \cite poling2001 <BR>
* See: R. Reid, et al.: The Properties of Gases and Liquids,
* 4th edition, McGraw-Hill, 1987, pp 396-397, 667
* 5th edition, McGraw-Hill, 2001, pp 9.7-9.8
*
* accentric factor taken from:
* Journal of Energy Resources Technology, March 2005, Vol 127
* Formulation for the Thermodynamic Properties
* Georeg A. Abediyi
* University, Mississippi State
* *
* V_c = (R*T_c)/p_c * Accentric factor taken from: <BR>
* Adebiyi (2003) \cite adebiyi2003
* *
*/ */
static Scalar gasViscosity(Scalar temperature, Scalar pressure) static Scalar gasViscosity(Scalar temperature, Scalar pressure)
...@@ -168,14 +161,12 @@ public: ...@@ -168,14 +161,12 @@ public:
/*! /*!
* \brief Specific enthalpy of air \f$\mathrm{[J/kg]}\f$ * \brief Specific enthalpy of air \f$\mathrm{[J/kg]}\f$
* with 273.15 K as basis. * with 273.15 \f$ K \f$ as basis. <BR>
* See:
* W. Kays, M. Crawford, B. Weigand
* Convective heat and mass transfer, 4th edition (2005)
* p. 431ff
* *
* \param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param temperature temperature of component in \f$\mathrm{[K]}\f$
* \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$
*
* Kays et al. (2005, 431ff) \cite kays2005 <BR>
*/ */
static Scalar gasEnthalpy(Scalar temperature, Scalar pressure) static Scalar gasEnthalpy(Scalar temperature, Scalar pressure)
{ {
...@@ -188,7 +179,7 @@ public: ...@@ -188,7 +179,7 @@ public:
* Definition of enthalpy: \f$h= u + pv = u + p / \rho\f$. * Definition of enthalpy: \f$h= u + pv = u + p / \rho\f$.
* Rearranging for internal energy yields: \f$u = h - pv\f$. * Rearranging for internal energy yields: \f$u = h - pv\f$.
* Exploiting the Ideal Gas assumption * Exploiting the Ideal Gas assumption
* (\f$pv = R_{\textnormal{specific}} T\f$)gives: \f$u = h - R / M T \f$. * (\f$pv = R_{\textnormal{specific}} T\f$) gives: \f$u = h - R / M T \f$.
* *
* \param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param temperature temperature of component in \f$\mathrm{[K]}\f$
* \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$
...@@ -210,12 +201,11 @@ public: ...@@ -210,12 +201,11 @@ public:
* This methods uses the formula for "zero-pressure" heat capacity that * This methods uses the formula for "zero-pressure" heat capacity that
* is only dependent on temperature, because the pressure dependence is rather small. * is only dependent on temperature, because the pressure dependence is rather small.
* This one should be accurate for a pressure of 1 atm. * This one should be accurate for a pressure of 1 atm.
* Values taken from NASA Contractor Report 4755, Real-Gas Flow Properties for NASA
* Langley Research Center Aerothermodynamic Facilities Complex Wind Tunnels
* using data from
* Hilsenrath et al 1955, "Tables of Thermal Properties of Gases"
* \param temperature temperature of component in \f$\mathrm{[K]}\f$ * \param temperature temperature of component in \f$\mathrm{[K]}\f$
* \param pressure pressure of component in \f$\mathrm{[Pa]}\f$ * \param pressure pressure of component in \f$\mathrm{[Pa]}\f$
*
* Values taken from Hollis (1996) \cite hollis1996 <BR>
* "Tables of Thermal Properties of Gases"
*/ */
static const Scalar gasHeatCapacity(Scalar temperature, static const Scalar gasHeatCapacity(Scalar temperature,
Scalar pressure) Scalar pressure)
...@@ -244,11 +234,10 @@ public: ...@@ -244,11 +234,10 @@ public:
/*! /*!
* \brief Thermal conductivity \f$\mathrm{[[W/(m*K)]}\f$ of air. * \brief Thermal conductivity \f$\mathrm{[[W/(m*K)]}\f$ of air.
* Isobaric Properties for Nitrogen in: NIST Standard * Isobaric Properties for Nitrogen in: NIST Standard \cite NIST <BR>
* see http://webbook.nist.gov/chemistry/fluid/ * evaluated at p=.1 MPa, T=20°C <BR>
* evaluated at p=.1 MPa, T=20°C * Nitrogen: 0.025398 <BR>
* Nitrogen: 0.025398 * Oxygen: 0.026105 <BR>
* Oxygen: 0.026105
* lambda_air is approximately 0.78*lambda_N2+0.22*lambda_O2 * lambda_air is approximately 0.78*lambda_N2+0.22*lambda_O2
*/ */
static Scalar gasThermalConductivity(Scalar temperature, Scalar pressure) static Scalar gasThermalConductivity(Scalar temperature, Scalar pressure)
......
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