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Remove non-ASCII characters
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@ -114,11 +114,11 @@ public:
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//- the dragfunction K used in the momentum eq.
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// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
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// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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// for numerical reasons alpha and beta has been
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// extracted from the dragFunction K,
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// so you MUST divide K by alpha*beta when implemnting the drag function
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
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};
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@ -114,12 +114,12 @@ public:
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//- the heat-transfer function K used in the enthalpy eq.
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// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
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// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB!*****************************
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// for numerical reasons alpha and beta has been
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// extracted from the heat-transfer function K,
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// so you MUST divide K by alpha*beta when implementing the
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// heat-transfer function
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB!*****************************
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virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
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};
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@ -35,8 +35,8 @@ Description
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\verbatim
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Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, Lindau. J.W.,
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Gibeling, H.J., Venkateswaran, S., Govindan, T.R.,
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“A Preconditioned Implicit Method for Two-Phase Flows with Application
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to Cavitation Prediction,”
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"A Preconditioned Implicit Method for Two-Phase Flows with Application
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to Cavitation Prediction,"
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Computers and Fluids,
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29(8):849-875, 2000.
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\endverbatim
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@ -131,11 +131,11 @@ public:
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//- the dragfunction K used in the momentum eq.
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// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
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// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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// for numerical reasons alpha and beta has been
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// extracted from the dragFunction K,
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// so you MUST divide K by alpha*beta when implemnting the drag function
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
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};
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@ -114,12 +114,12 @@ public:
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//- the heat-transfer function K used in the enthalpy eq.
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// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
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// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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// for numerical reasons alpha and beta has been
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// extracted from the heat-transfer function K,
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// so you MUST divide K by alpha*beta when implementing the
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// heat-transfer function
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB! *****************************
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virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
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};
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@ -114,11 +114,11 @@ public:
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//- the dragfunction K used in the momentum eq.
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// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
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// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB ! *****************************
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// for numerical reasons alpha and beta has been
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// extracted from the dragFunction K,
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// so you MUST divide K by alpha*beta when implemnting the drag function
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// **********************************<EFBFBD>NB ! *****************************
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// ********************************** NB ! *****************************
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virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
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};
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