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basic.H
XiModel.H SCOPELaminarFlameSpeed.H basicXiSubXiEq.H basicXiSubG.H Doxyfile (include PATH to OpenCFD Macros) doxyFilt (include class documentation in /src)
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@ -29,6 +29,33 @@ Description
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Basic sub-grid obstacle flame-wrinking enhancement factor model.
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Details supplied by J Puttock 2/7/06.
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Sub-grid flame area generation
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\f$ n = N - \hat{\dwea{\vec{U}}}.n_{s}.\hat{\dwea{\vec{U}}} \f$
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\f$ n_{r} = \sqrt{n} \f$
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where:
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\f$ \hat{\dwea{\vec{U}}} = \dwea{\vec{U}} / \vert \dwea{\vec{U}}
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\vert \f$
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\f$ b = \hat{\dwea{\vec{U}}}.B.\hat{\dwea{\vec{U}}} / n_{r} \f$
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where
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\f$ B \f$ is the file "B".
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\f$ N \f$ is the file "N".
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\f$ n_{s} \f$ is the file "ns".
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The flame area enhancement factor \f$ \Xi_{sub} \f$ is expected to
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approach:
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\f[ \Xi_{{sub}_{eq}} = 1 + max(2.2 \sqrt{b}, min(0.34 \frac{\vert \dwea{\vec{U}}
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\vert}{{\vec{U}}^{'}}, 1.6)) \times min(\frac{n}{4}, 1) \f]
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SourceFiles
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basicSubGrid.C
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@ -25,10 +25,28 @@ License
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Class
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basicSubGrid
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Description
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Basic sub-grid obstacle flame-wrinking generation rate coefficient model.
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Details supplied by J Puttock 2/7/06.
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\f$ G_{sub} \f$ denotes the generation coefficient and it is given by
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\f[
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G_{sub} = k_{1} /frac{\vert \dwea{\vec{U}} \vert}{L_{obs}}
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\frac{/Xi_{{sub}_{eq}}-1}{/Xi_{sub}}
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\f]
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and the removal:
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\f[ - k_{1} /frac{\vert \dwea{\vec{U}} \vert}{L_{sub}}
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\frac{\Xi_{sub}-1}{\Xi_{sub}} \f]
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Finally, \f$ G_{sub} \f$ is added to generation rate \f$ G_{in} \f$
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due to the turbulence.
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SourceFiles
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basicSubGrid.C
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@ -29,6 +29,45 @@ Description
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Basic sub-grid obstacle drag model.
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Details supplied by J Puttock 2/7/06.
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Sub-grid drag term
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The resistance term (force per unit of volume) is given by:
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\f[
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R = -\frac{1}{2} \rho \vert \dwea{\vec{U}} \vert \dwea{\vec{U}}.D
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\f]
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where:
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\f$ D \f$ is the tensor field "CR" in \f$ m^{-1} \f$
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This is term is treated implicitly in UEqn.H
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Sub-grid turbulence generation
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The turbulence source term \f$ G_{R} \f$ occurring in the
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\f$ \kappa-\epsilon \f$ equations for the generation of turbulence due to interaction with unresolved obstacles :
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\f$ G_{R} = C_{s}\beta_{\nu} \mu_{eff} A_{w}^{2}(\dwea{\vec{U}}-\dwea{\vec{U}_{s}})^2 + \frac{1}{2}
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\rho \vert \dwea{\vec{U}} \vert \dwea{\vec{U}}.T.\dwea{\vec{U}} \f$
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where:
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\f$ C_{s} \f$ = 1
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\f$ \beta_{\nu} \f$ is the volume porosity (file "betav").
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\f$ \mu_{eff} \f$ is the effective viscosity.
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\f$ A_{w}^{2}\f$ is the obstacle surface area per unit of volume (file "Aw").
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\f$ \dwea{\vec{U}_{s}} \f$ is the slip velocity and is considered \f$ \frac{1}{2}. \dwea{\vec{U}} \f$.
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\f$ T \f$ is a tensor in the file CT.
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The term \f$ G_{R} \f$ is treated explicitly in the \f$ \kappa-\epsilon \f$ Eqs in the PDRkEpsilon.C file.
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SourceFiles
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basic.C
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@ -40,7 +79,6 @@ SourceFiles
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#include "PDRDragModel.H"
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#include "XiEqModel.H"
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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namespace Foam
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{
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@ -27,6 +27,53 @@ Class
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Description
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Base-class for all Xi models used by the b-Xi combustion model.
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See Technical Report SH/RE/01R for details on the PDR modelling.
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Xi is given through an algebraic expression (algebraic.H), by solving a transport equation (transport.H) or a fixed value (fixed.H). See report
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TR/HGW/10 for details on the Weller two equations model.
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In the algebraic and transport methods \f$\Xi_{eq}\f$ is calculated in
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similar way. In the algebraic approach, \f$\Xi_{eq}\f$ is the value used in
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the \f$ b \f$ transport equation.
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\f$\Xi_{eq}\f$ is calculated as follows:
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\f$\Xi_{eq} = 1 + (1 + 2\Xi_{coeff}(0.5 - \dwea{b}))(\Xi^* - 1)\f$
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where:
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\f$ \dwea{b} \f$ is the regress variable.
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\f$ \Xi^* \f$ is the total equilibrium wrinkling combining the effects
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of the flame inestability and turbulence interaction and is given by
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\f[
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\Xi^* = \frac {R}{R - G_\eta - G_{in}}
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\f]
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where:
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\f$ G_\eta \f$ is the generation rate of wrinkling due to turbulence interaction.
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\f$ G_{in} = \kappa \rho_{u}/\rho_{b} \f$ is the generation
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rate due to the flame inestability.
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By adding the removal rates of the two effects:
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\f[
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R = G_\eta \frac{\Xi_{\eta_{eq}}}{\Xi_{\eta_{eq}} - 1}
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+ G_{in} \frac{\Xi_{{in}_{eq}}}{\Xi_{{in}_{eq}} - 1}
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\f]
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where:
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\f$ R \f$ is the total removal.
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\f$ G_\eta \f$ is a model constant.
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\f$ \Xi_{\eta_{eq}} \f$ is the flame wrinkling due to turbulence.
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\f$ \Xi_{{in}_{eq}} \f$ is the equilibrium level of the flame wrinkling generated by inestability. It is a constant (default 2.5).
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SourceFiles
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XiModel.C
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@ -51,6 +98,8 @@ namespace Foam
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Class XiModel Declaration
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\*---------------------------------------------------------------------------*/
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class XiModel
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{
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@ -28,6 +28,25 @@ Class
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Description
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Laminar flame speed obtained from the SCOPE correlation.
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Seven parameters are specified in terms of polynomial functions of stoichiometry. Two polynomials are fitted, covering different parts of the flammable range. If the mixture is outside the fitted range, linear interpolation is used between the extreme of the polynomio and the upper or lower flammable limit with the Markstein number constant.
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Variations of pressure and temperature from the reference values are taken into account through \f$ pexp \f$ and \f$ texp \f$
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The laminar burning velocity fitting polynomio is:
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\f$ Su = a_{0}(1+a_{1}x+K+..a_{i}x^{i}..+a_{6}x^{6}) (p/p_{ref})^{pexp} (T/T_{ref})^{texp} \f$
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where:
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\f$ a_{i} \f$ are the polinomial coefficients.
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\f$ pexp \f$ and \f$ texp \f$ are the pressure and temperature factors respectively.
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\f$ x \f$ is the equivalence ratio.
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\f$ T_{ref} \f$ and \f$ p_{ref} \f$ are the temperature and pressure references for the laminar burning velocity.
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SourceFiles
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SCOPELaminarFlameSpeed.C
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@ -50,9 +50,9 @@ then
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*/applications/solvers/*.C | */applications/utilities/*.C )
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awkScript=$WM_PROJECT_DIR/bin/tools/doxyFilt-top.awk
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;;
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*/applications/solvers/*.H | */applications/utilities/*.H )
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awkScript=$WM_PROJECT_DIR/bin/tools/doxyFilt-ignore.awk
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;;
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# */applications/solvers/*.H | */applications/utilities/*.H )
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# awkScript=$WM_PROJECT_DIR/bin/tools/doxyFilt-ignore.awk
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# ;;
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esac
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awk -f $awkScript $1 | \
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@ -14,6 +14,16 @@
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# Project related configuration options
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#---------------------------------------------------------------------------
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#--------------------------------
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# PATH FOR OPEN CFD LATEX MACROS
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#-------------------------------
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@INLUDE_PATH = $(TEXINPUTS)
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@INLUDE_PATH += $(BIBINPUTS)
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@INLUDE_PATH += $(BSTINPUTS)
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# This tag specifies the encoding used for all characters in the config file that
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# follow. The default is UTF-8 which is also the encoding used for all text before
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# the first occurrence of this tag. Doxygen uses libiconv (or the iconv built into
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@ -477,9 +487,14 @@ WARN_LOGFILE =
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# directories like "/usr/src/myproject". Separate the files or directories
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# with spaces.
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INPUT = $(WM_PROJECT_DIR)/src \
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$(WM_PROJECT_DIR)/applications/utilities \
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$(WM_PROJECT_DIR)/applications/solvers
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INPUT = $(WM_PROJECT_DIR)/applications/solvers/combustion/PDRFoam
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#$(WM_PROJECT_DIR)/applications/solvers/combustion \
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#$(WM_PROJECT_DIR)/src/thermophysicalModels/laminarFlameSpeed
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#$(WM_PROJECT_DIR)/applications/utilities \
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#$(WM_PROJECT_DIR)/applications/solvers/combustion/PDRFoam
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# This tag can be used to specify the character encoding of the source files that
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# doxygen parses. Internally doxygen uses the UTF-8 encoding, which is also the default
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@ -536,7 +551,9 @@ EXCLUDE_SYMBOLS =
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# directories that contain example code fragments that are included (see
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# the \include command).
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EXAMPLE_PATH =
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EXAMPLE_PATH = $(TEXINPUTS) \
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$(BIBINPUTS) \
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$(BSTINPUTS)
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# If the value of the EXAMPLE_PATH tag contains directories, you can use the
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# EXAMPLE_PATTERNS tag to specify one or more wildcard pattern (like *.cpp
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@ -824,7 +841,8 @@ PAPER_TYPE = a4wide
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# The EXTRA_PACKAGES tag can be to specify one or more names of LaTeX
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# packages that should be included in the LaTeX output.
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EXTRA_PACKAGES =
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EXTRA_PACKAGES = conditionalEqns finiteVolume algorithmic tensorCommon \
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tensorOperator tensorEquation
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# The LATEX_HEADER tag can be used to specify a personal LaTeX header for
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# the generated latex document. The header should contain everything until
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