From 2180566078f8bc95bb68f4ab0dcd4d9a0357914a Mon Sep 17 00:00:00 2001 From: Michael Wild Date: Wed, 18 Jan 2012 21:58:48 +0100 Subject: [PATCH] STYLE: Non-ascii characters and typos in comments Signed-off-by: Michael Wild --- .../dragModels/dragModel/dragModel.H | 10 +++++----- .../heatTransferModel/heatTransferModel.H | 11 +++++------ .../phaseChangeTwoPhaseMixtures/Kunz/Kunz.H | 4 ++-- .../dragModels/dragModel/dragModel.H | 10 +++++----- .../heatTransferModel/heatTransferModel.H | 11 +++++------ .../dragModels/dragModel/dragModel.H | 10 +++++----- .../molecule/reducedUnits/reducedUnits.H | 2 +- .../old/reducedUnits/reducedUnits.H | 2 +- .../RAS/SpalartAllmaras/SpalartAllmaras.H | 2 +- .../RAS/SpalartAllmaras/SpalartAllmaras.H | 2 +- 10 files changed, 31 insertions(+), 33 deletions(-) diff --git a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H index 6d2add9..63df1ce 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 ! ***************************** - // 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 ! ***************************** + // for numerical reasons alpha and beta has been extracted from the + // dragFunction K, so you MUST divide K by alpha*beta when implementing + // the drag function + // ********************************** 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 e4871f2..ad5de57 100644 --- a/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H +++ b/applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H @@ -114,12 +114,11 @@ 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 ! ***************************** - // 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 ! ***************************** + // 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 ! ***************************** 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 31ea816..74f8f2b 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 a775d91..9131558 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 ! ***************************** - // 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 ! ***************************** + // for numerical reasons alpha and beta has been extracted from the + // dragFunction K, so you MUST divide K by alpha*beta when implementing + // the drag function + // ********************************** 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 e4871f2..ad5de57 100644 --- a/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H +++ b/applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H @@ -114,12 +114,11 @@ 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 ! ***************************** - // 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 ! ***************************** + // 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 ! ***************************** 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 237c7cf..e96a9a8 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 ! ***************************** - // 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 ! ***************************** + // for numerical reasons alpha and beta has been extracted from the + // dragFunction K, so you MUST divide K by alpha*beta when implementing + // the drag function + // ********************************** 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 632e5d3..330bca1 100644 --- a/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H +++ b/src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H @@ -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(); diff --git a/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H b/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H index 632e5d3..330bca1 100644 --- a/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H +++ b/src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H @@ -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(); diff --git a/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H b/src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H index 9faed12..3ed218e 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 f310478..50d3184 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: -- 1.7.5.4