diff --git a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H index 6d2add98f9..97c9d455f1 100644 --- a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H +++ b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H @@ -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) - // **********************************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 - // **********************************NB ! ***************************** + // ********************************** NB! ***************************** virtual tmp K(const volScalarField& Ur) const = 0; }; diff --git a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H index e4871f2c51..f83a03804b 100644 --- a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H +++ b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H @@ -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) - // **********************************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 - // **********************************NB ! ***************************** + // ********************************** NB!***************************** virtual tmp K(const volScalarField& Ur) const = 0; }; diff --git a/applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H b/applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H index 31ea8164df..74f8f2b931 100644 --- a/applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H +++ b/applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H @@ -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 diff --git a/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H b/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H index a775d91e45..3a9536c881 100644 --- a/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H +++ b/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H @@ -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) - // **********************************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 - // **********************************NB ! ***************************** + // ********************************** NB! ***************************** virtual tmp K(const volScalarField& Ur) const = 0; }; diff --git a/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H b/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H index e4871f2c51..5541795bfd 100644 --- a/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H +++ b/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H @@ -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) - // **********************************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 - // **********************************NB ! ***************************** + // ********************************** NB! ***************************** virtual tmp K(const volScalarField& Ur) const = 0; }; diff --git a/applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H b/applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H index 237c7cfb64..0831f158b6 100644 --- a/applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H +++ b/applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H @@ -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) - // **********************************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 - // **********************************NB ! ***************************** + // ********************************** NB ! ***************************** virtual tmp K(const volScalarField& Ur) const = 0; }; diff --git a/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H b/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H index 632e5d37ad..8319bf50bc 100644 --- a/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H +++ b/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H @@ -76,7 +76,7 @@ class reducedUnits scalar refPressure_; - scalar refMassDensity_; + scalar refMassDensity_; scalar refNumberDensity_; @@ -103,9 +103,9 @@ public: // Constructors //- Construct with no argument, uses default values: - // length = 1nm - // mass = 1.660538782e−27kg (unified atomic mass unit) - // temperature = 1K (therefore, energy = 1*kb) + // length = 1nm + // mass = 1.660538782e-27kg (unified atomic mass unit) + // temperature = 1K (therefore, energy = 1*kb) reducedUnits(); //- Construct from components diff --git a/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H b/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H index 632e5d37ad..8319bf50bc 100644 --- a/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H +++ b/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H @@ -76,7 +76,7 @@ class reducedUnits scalar refPressure_; - scalar refMassDensity_; + scalar refMassDensity_; scalar refNumberDensity_; @@ -103,9 +103,9 @@ public: // Constructors //- Construct with no argument, uses default values: - // length = 1nm - // mass = 1.660538782e−27kg (unified atomic mass unit) - // temperature = 1K (therefore, energy = 1*kb) + // length = 1nm + // mass = 1.660538782e-27kg (unified atomic mass unit) + // temperature = 1K (therefore, energy = 1*kb) reducedUnits(); //- Construct from components diff --git a/src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H b/src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H index d0891c14d1..a003e7bbc7 100644 --- a/src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H +++ b/src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H @@ -77,10 +77,10 @@ class tetOverlapVolume ); - //- Helping cľasses + //- Helper classes class dummyTetOp { - public: + public: inline void operator()(const tetPoints&){} }; @@ -88,7 +88,8 @@ class tetOverlapVolume class sumTetVolOp { - public: + public: + scalar vol_; inline sumTetVolOp() @@ -108,7 +109,7 @@ class tetOverlapVolume FixedList& tets_; label& nTets_; - public: + public: inline storeTetOp(FixedList& tets, label& nTets) : @@ -178,7 +179,7 @@ public: //- Destructor - virtual ~tetOverlapVolume(); + virtual ~tetOverlapVolume(); // Public members @@ -210,7 +211,6 @@ public: } // End namespace Foam - // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // #endif diff --git a/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H b/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H index 9faed1215c..f3b83a1148 100644 --- a/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H +++ b/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H @@ -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: diff --git a/src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H b/src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H index f3104787ab..fbd1248181 100644 --- a/src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H +++ b/src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H @@ -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: