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Remove non-ASCII characters
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@ -76,7 +76,7 @@ class reducedUnits
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scalar refPressure_;
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scalar refMassDensity_;
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scalar refMassDensity_;
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scalar refNumberDensity_;
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@ -103,9 +103,9 @@ public:
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// Constructors
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//- Construct with no argument, uses default values:
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// length = 1nm
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// mass = 1.660538782eâ27kg (unified atomic mass unit)
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// temperature = 1K (therefore, energy = 1*kb)
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// length = 1nm
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// mass = 1.660538782e-27kg (unified atomic mass unit)
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// temperature = 1K (therefore, energy = 1*kb)
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reducedUnits();
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//- Construct from components
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@ -76,7 +76,7 @@ class reducedUnits
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scalar refPressure_;
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scalar refMassDensity_;
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scalar refMassDensity_;
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scalar refNumberDensity_;
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@ -103,9 +103,9 @@ public:
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// Constructors
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//- Construct with no argument, uses default values:
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// length = 1nm
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// mass = 1.660538782eâ27kg (unified atomic mass unit)
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// temperature = 1K (therefore, energy = 1*kb)
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// length = 1nm
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// mass = 1.660538782e-27kg (unified atomic mass unit)
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// temperature = 1K (therefore, energy = 1*kb)
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reducedUnits();
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//- Construct from components
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@ -77,10 +77,10 @@ class tetOverlapVolume
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);
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//- Helping cľasses
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//- Helper classes
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class dummyTetOp
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{
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public:
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public:
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inline void operator()(const tetPoints&){}
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};
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@ -88,7 +88,8 @@ class tetOverlapVolume
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class sumTetVolOp
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{
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public:
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public:
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scalar vol_;
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inline sumTetVolOp()
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@ -108,7 +109,7 @@ class tetOverlapVolume
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FixedList<tetPoints, 200>& tets_;
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label& nTets_;
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public:
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public:
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inline storeTetOp(FixedList<tetPoints, 200>& tets, label& nTets)
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:
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@ -178,7 +179,7 @@ public:
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//- Destructor
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virtual ~tetOverlapVolume();
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virtual ~tetOverlapVolume();
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// Public members
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@ -210,7 +211,6 @@ public:
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} // End namespace Foam
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#endif
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@ -33,7 +33,7 @@ Description
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"A One-Equation Turbulence Model for Aerodynamic Flows"
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P.R. Spalart,
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S.R. Allmaras,
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La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
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La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
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Extended according to:
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@ -33,7 +33,7 @@ Description
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"A One-Equation Turbulence Model for Aerodynamic Flows"
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P.R. Spalart,
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S.R. Allmaras,
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La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
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La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
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Extended according to:
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