zhyang-dev/openfoam
1
0
Fork 0
mirror of https://develop.openfoam.com/Development/openfoam.git synced 2025-11-28 03:28:01 +00:00
Code Issues Actions Packages Projects Releases Wiki Activity

Remove non-ASCII characters

Browse Source
This commit is contained in:
Henry
2012-01-19 16:27:23 +00:00
parent fa9eb43280
commit 0b1bcbb753
11 changed files with 28 additions and 28 deletions
Download Patch File Download Diff File Expand all files Collapse all files

4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
View File

@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB!*****************************
// for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the
// heat-transfer function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB!*****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H
View File

@ -35,8 +35,8 @@ Description
\verbatim
Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, Lindau. J.W.,
Gibeling, H.J., Venkateswaran, S., Govindan, T.R.,
“A Preconditioned Implicit Method for Two-Phase Flows with Application
to Cavitation Prediction,”
"A Preconditioned Implicit Method for Two-Phase Flows with Application
to Cavitation Prediction,"
Computers and Fluids,
29(8):849-875, 2000.
\endverbatim

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -131,11 +131,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
View File

@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the
// heat-transfer function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB ! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB ! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

2
src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H
View File

@ -104,7 +104,7 @@ public:
//- Construct with no argument, uses default values:
// length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit)
// mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb)
reducedUnits();

2
src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H
View File

@ -104,7 +104,7 @@ public:
//- Construct with no argument, uses default values:
// length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit)
// mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb)
reducedUnits();

4
src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H
View File

@ -77,7 +77,7 @@ class tetOverlapVolume
);
//- Helping cľasses
//- Helper classes
class dummyTetOp
{
public:
@ -89,6 +89,7 @@ class tetOverlapVolume
class sumTetVolOp
{
public:
scalar vol_;
inline sumTetVolOp()
@ -210,7 +211,6 @@ public:
} // End namespace Foam
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#endif

2
src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H
View File

@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart,
S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to:

2
src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H
View File

@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart,
S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to: