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STYLE: backslash doxygen commands, email address, typos in error messages
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@ -31,7 +31,7 @@ Description
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corresponding to PDR basic drag model (\link basic.H \endlink)
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The default model coefficients correspond to the following:
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@verbatim
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\verbatim
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PDRkEpsilonCoeffs
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{
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Cmu 0.09;
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@ -43,7 +43,7 @@ Description
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sigmaEps 1.3;
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Prt 1.0; // only for compressible
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}
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@endverbatim
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\endverbatim
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The turbulence source term \f$ G_{R} \f$ appears in the
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\f$ \kappa-\epsilon \f$ equation for the generation of turbulence due to
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@ -29,7 +29,7 @@ Class
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Description
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Simple SCOPEBlendXiEq model for XiEq based on SCOPEXiEqs correlation
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with a linear correction function to give a plausible profile for XiEq.
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See @link SCOPELaminarFlameSpeed.H @endlink for details on the SCOPE
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See \link SCOPELaminarFlameSpeed.H \endlink for details on the SCOPE
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laminar flame speed model.
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SourceFiles
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@ -29,7 +29,7 @@ Class
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Description
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This is the equilibrium level of the flame wrinkling generated by
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instability. It is a constant (default 2.5). It is used in
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@link XiModel.H @endlink.
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\link XiModel.H \endlink.
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SourceFiles
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instability.C
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@ -41,8 +41,7 @@ Description
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airframe noise, VKI LS 2013-03.
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\endverbatim
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Contact: info@cfd-berlin.com
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Contact: info@upstream-cfd.com
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\*---------------------------------------------------------------------------*/
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@ -816,7 +816,7 @@ void correctCoupledBoundaryConditions(fvMesh& mesh)
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -46,8 +46,8 @@ Description
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}
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\endverbatim
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The result program would receive \b -time, @b -latestTime, @b -constant
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and \b -noZero options. The @b -constant option explicitly includes the
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The result program would receive \b -time, \b -latestTime, \b -constant
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and \b -noZero options. The \b -constant option explicitly includes the
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\c constant/ directory in the time list and the \b -noZero option
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explicitly excludes the \c 0/ directory from the time list.
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@ -133,7 +133,7 @@ public:
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// behaviour (and \b -latestTime behaviour) to exclude the \c 0/
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// directory. The \c 0/ directory will only be included when
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// \b -withZero is specified.
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// The \b -noZero option has precedence over the @b -withZero option.
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// The \b -noZero option has precedence over the \b -withZero option.
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static void addOptions
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(
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const bool constant=true,
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@ -432,7 +432,7 @@ evaluate()
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -91,7 +91,7 @@ void Foam::LduMatrix<Type, DType, LUType>::initMatrixInterfaces
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -200,7 +200,7 @@ void Foam::LduMatrix<Type, DType, LUType>::updateMatrixInterfaces
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -92,7 +92,7 @@ void Foam::lduMatrix::initMatrixInterfaces
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -272,7 +272,7 @@ void Foam::lduMatrix::updateMatrixInterfaces
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else
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{
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FatalErrorInFunction
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<< "Unsuported communications type "
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<< "Unsupported communications type "
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<< Pstream::commsTypeNames[Pstream::defaultCommsType]
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<< exit(FatalError);
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}
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@ -33,17 +33,19 @@ Description
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Primary Breakup Model for pressure swirl atomizers.
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Accurate description in
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@verbatim
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\verbatim
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Z. Han, S. Parrish, P.V. Farrell, R.D. Reitz
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"Modeling Atomization Processes Of Pressure Swirl Hollow-Cone Fuel Sprays"
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Atomization and Sprays, vol. 7, pp. 663-684, 1997
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\endverbatim
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and
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\verbatim
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L. Allocca, G. Bella, A. De Vita, L. Di Angelo
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"Experimental Validation of a GDI Spray Model"
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SAE Technical Paper Series, 2002-01-1137
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@endverbatim
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\endverbatim
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\*---------------------------------------------------------------------------*/
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@ -57,6 +59,7 @@ Description
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class BlobsSheetAtomization Declaration
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\*---------------------------------------------------------------------------*/
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@ -33,19 +33,19 @@ Description
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Primary Breakup Model for pressure swirl atomizers.
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Accurate description in
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@verbatim
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\verbatim
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P.K. Senecal, D.P. Schmidt, I. Nouar, C.J. Rutland, R.D. Reitz, M. Corradini
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"Modeling high-speed viscous liquid sheet atomization"
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International Journal of Multiphase Flow 25 (1999) pags. 1073-1097
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@endverbatim
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\endverbatim
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and
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@verbatim
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\verbatim
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D.P. Schmidt, I. Nouar, P.K. Senecal, C.J. Rutland, J.K. Martin, R.D. Reitz
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"Pressure-Swirl Atomization in the Near Field"
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SAE Techical Paper Series 1999-01-0496
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@endverbatim
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\endverbatim
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\*---------------------------------------------------------------------------*/
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@ -58,6 +58,7 @@ Description
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class LISAAtomization Declaration
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\*---------------------------------------------------------------------------*/
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@ -33,7 +33,7 @@ Description
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The Enhanced TAB model.
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Described in the papers below.
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@verbatim
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\verbatim
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F.X. Tanner
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"Liquid Jet Atomization and Droplet Breakup Modeling of
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Non-Evaporating Diesel Fuel Sprays"
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@ -45,7 +45,7 @@ Description
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Fuel Sprays by Means of Cascade Drop Breakup Model"
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SAE 980808
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SAE Technical Paper Series
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@endverbatim
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\endverbatim
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See also
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The TAB model
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@ -61,6 +61,7 @@ See also
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class ETAB Declaration
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\*---------------------------------------------------------------------------*/
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@ -32,13 +32,13 @@ Group
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Description
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Particle secondary breakup model, based on the reference:
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@verbatim
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\verbatim
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Pilch, M. and Erdman, C.A.
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"Use of breakup time data and velocity history data
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to predict the maximum size of stable fragments for acceleration
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induced breakup of a liquid drop."
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Int. J. Multiphase Flows 13 (1987), 741-757
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@endverbatim
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\endverbatim
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The droplet fragment velocity is described by the equation:
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@ -69,6 +69,7 @@ Description
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class PilchErdman Declaration
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\*---------------------------------------------------------------------------*/
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@ -32,23 +32,23 @@ Group
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Description
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secondary breakup model
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@verbatim
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\verbatim
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Reitz, R.D.
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"Modelling atomization processes in highpressure vaporizing sprays"
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Atomization and Spray Technology 3 (1987), 309-337
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@endverbatim
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\endverbatim
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@verbatim
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\verbatim
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Reitz, R.D. and Diwakar, R.
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"Effect of drop breakup on fuel sprays"
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SAE Tech. paper series, 860469 (1986)
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@endverbatim
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\endverbatim
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@verbatim
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\verbatim
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Reitz, R.D. and Diwakar, R.
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"Structure of high-pressure fuel sprays"
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SAE Tech. paper series, 870598 (1987)
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@endverbatim
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\endverbatim
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\*---------------------------------------------------------------------------*/
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@ -61,6 +61,7 @@ Description
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class ReitzDiwakar Declaration
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\*---------------------------------------------------------------------------*/
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@ -34,12 +34,12 @@ Description
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bag, molutimode, shear....
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Accurate description in
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@verbatim
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\verbatim
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R. Schmehl, G. Maier, S. Witting
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"CFD Analysis of Fuel Atomization, Secondary Droplet Breakup and Spray
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Dispersion in the Premix Duct of a LPP Combustor".
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Eight International Conference on Liquid Atomization and Spray Systems, 2000
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@endverbatim
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\endverbatim
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\*---------------------------------------------------------------------------*/
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@ -52,6 +52,7 @@ Description
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class SHF Declaration
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\*---------------------------------------------------------------------------*/
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@ -32,14 +32,14 @@ Group
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Description
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The TAB Method for Numerical Calculation of Spray Droplet Breakup.
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@verbatim
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\verbatim
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O'Rourke, P.J. and Amsden, A.A.,
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"The TAB Method for Numerical Calculation of Spray Droplet Breakup,"
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1987 SAE International Fuels and Lubricants Meeting and Exposition,
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Toronto, Ontario, November 2-5, 1987,
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Los Alamos National Laboratory document LA-UR-87-2105;
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SAE Technical Paper Series, Paper 872089.
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@endverbatim
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\endverbatim
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This implementation follows the kiva version.
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@ -58,6 +58,7 @@ See also
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namespace Foam
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{
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/*---------------------------------------------------------------------------*\
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Class TAB Declaration
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\*---------------------------------------------------------------------------*/
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Reference in New Issue
Block a user