Corrected typos in comments

found using cspell.

Patch contributed by Timo Niemi, VTT.
This commit is contained in:
Henry Weller
2019-10-18 11:46:20 +01:00
parent 7ec1f0d6a8
commit 81fca4c43a
167 changed files with 268 additions and 267 deletions

View File

@ -25,7 +25,7 @@ Class
Foam::XiEqModels::basicSubGrid
Description
Basic sub-grid obstacle flame-wrinking enhancement factor model.
Basic sub-grid obstacle flame-wrinkling enhancement factor model.
Details supplied by J Puttock 2/7/06.
<b> Sub-grid flame area generation </b>
@ -119,7 +119,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const;
//- Update properties from given dictionary

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@ -26,7 +26,7 @@ Class
Description
Basic sub-grid obstacle flame-wrinking generation rate coefficient model.
Basic sub-grid obstacle flame-wrinkling generation rate coefficient model.
Details supplied by J Puttock 2/7/06.
\f$ G_{sub} \f$ denotes the generation coefficient and it is given by
@ -107,7 +107,7 @@ public:
// Member Functions
//- Return the flame-wrinking generation rate
//- Return the flame-wrinkling generation rate
virtual tmp<volScalarField> G() const;
//- Return the flame diffusivity

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -129,7 +129,7 @@ void PDRkEpsilon::correct()
volScalarField G(GName(), rho_*nut_*(tgradU() && dev(twoSymm(tgradU()))));
tgradU.clear();
// Update espsilon and G at the wall
// Update epsilon and G at the wall
epsilon_.boundaryFieldRef().updateCoeffs();
// Add the blockage generation term so that it is included consistently

View File

@ -95,7 +95,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const;
//- Update properties from given dictionary

View File

@ -91,7 +91,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const;
//- Update properties from given dictionary

View File

@ -109,7 +109,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const;
//- Update properties from given dictionary

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@ -136,7 +136,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const
{
return turbulence_.muEff();

View File

@ -90,7 +90,7 @@ public:
// Member Functions
//- Return the flame-wrinking XiEq
//- Return the flame-wrinkling XiEq
virtual tmp<volScalarField> XiEq() const;
//- Update properties from given dictionary

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@ -25,7 +25,7 @@ Class
Foam::XiGModels::KTS
Description
Simple Kolmogorov time-scale (KTS) model for the flame-wrinling generation
Simple Kolmogorov time-scale (KTS) model for the flame-wrinkling generation
rate.
SourceFiles
@ -85,7 +85,7 @@ public:
// Member Functions
//- Return the flame-wrinking generation rate
//- Return the flame-wrinkling generation rate
virtual tmp<volScalarField> G() const;
//- Update properties from given dictionary

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@ -127,7 +127,7 @@ public:
// Member Functions
//- Return the flame-wrinking generation rate
//- Return the flame-wrinkling generation rate
virtual tmp<volScalarField> G() const = 0;
//- Return the flame diffusivity

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@ -25,7 +25,7 @@ Class
Foam::XiGModels::instabilityG
Description
Flame-surface instabilityG flame-wrinking generation rate coefficient model
Flame-surface instabilityG flame-wrinkling generation rate coefficient model
used in \link XiModel.H \endlink.
See Technical Report SH/RE/01R for details on the PDR modelling.
@ -57,7 +57,7 @@ class instabilityG
{
// Private Data
//- Flame instabilityG wrinling generation rate coefficient
//- Flame instabilityG wrinkling generation rate coefficient
dimensionedScalar GIn_;
//- InstabilityG length-scale
@ -94,7 +94,7 @@ public:
// Member Functions
//- Return the flame-wrinking generation rate
//- Return the flame-wrinkling generation rate
virtual tmp<volScalarField> G() const;
//- Return the flame diffusivity

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@ -49,7 +49,7 @@ Description
\f$ \Xi_{coeff} \f$ is a model constant.
\f$ \Xi^* \f$ is the total equilibrium wrinkling combining the effects
of the flame inestability and turbulence interaction and is given by
of the flame instability and turbulence interaction and is given by
\f[
\Xi^* = \frac {R}{R - G_\eta - G_{in}}
@ -61,7 +61,7 @@ Description
interaction.
\f$ G_{in} = \kappa \rho_{u}/\rho_{b} \f$ is the generation
rate due to the flame inestability.
rate due to the flame instability.
By adding the removal rates of the two effects:
@ -79,7 +79,7 @@ Description
\f$ \Xi_{\eta_{eq}} \f$ is the flame wrinkling due to turbulence.
\f$ \Xi_{{in}_{eq}} \f$ is the equilibrium level of the flame wrinkling
generated by inestability. It is a constant (default 2.5).
generated by instability. It is a constant (default 2.5).
SourceFiles
@ -122,7 +122,7 @@ protected:
const volScalarField& b_;
const surfaceScalarField& phi_;
//- Flame wrinking field
//- Flame wrinkling field
volScalarField Xi_;
@ -199,7 +199,7 @@ public:
// Member Functions
//- Return the flame-wrinking Xi
//- Return the flame-wrinkling Xi
virtual const volScalarField& Xi() const
{
return Xi_;
@ -219,10 +219,10 @@ public:
)
{}
//- Correct the flame-wrinking Xi
//- Correct the flame-wrinkling Xi
virtual void correct() = 0;
//- Correct the flame-wrinking Xi using the given convection scheme
//- Correct the flame-wrinkling Xi using the given convection scheme
virtual void correct(const fv::convectionScheme<scalar>&)
{
correct();

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@ -98,7 +98,7 @@ public:
//- Return the flame diffusivity
virtual tmp<volScalarField> Db() const;
//- Correct the flame-wrinking Xi
//- Correct the flame-wrinkling Xi
virtual void correct();
//- Update properties from given dictionary

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@ -83,7 +83,7 @@ public:
// Member Functions
//- Correct the flame-wrinking Xi
//- Correct the flame-wrinkling Xi
virtual void correct()
{}

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@ -107,13 +107,13 @@ public:
fields.add(Xi_);
}
//- Correct the flame-wrinking Xi
//- Correct the flame-wrinkling Xi
virtual void correct()
{
NotImplemented;
}
//- Correct the flame-wrinking Xi using the given convection scheme
//- Correct the flame-wrinkling Xi using the given convection scheme
virtual void correct(const fv::convectionScheme<scalar>& mvConvection);
//- Update properties from given dictionary

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@ -30,7 +30,7 @@ Description
Seven parameters are specified in terms of polynomial functions of
stoichiometry. Two polynomials are fitted, covering different parts of the
flammable range. If the mixture is outside the fitted range, linear
interpolation is used between the extreme of the polynomio and the upper or
interpolation is used between the extreme of the polynomial and the upper or
lower flammable limit with the Markstein number constant.
Variations of pressure and temperature from the reference values are taken
@ -43,7 +43,7 @@ Description
where:
\f$ a_{i} \f$ are the polinomial coefficients.
\f$ a_{i} \f$ are the polynomial coefficients.
\f$ pexp \f$ and \f$ texp \f$ are the pressure and temperature factors
respectively.
@ -109,10 +109,10 @@ class SCOPE
dictionary coeffsDict_;
//- Lower flamability limit
//- Lower flammability limit
scalar LFL_;
//- Upper flamability limit
//- Upper flammability limit
scalar UFL_;
//- Lower Su polynomial

View File

@ -114,7 +114,7 @@ public:
return relativePermeability_;
}
//- Return remenence
//- Return remanence
inline const dimensionedScalar& Mr() const
{
return remanence_;

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@ -1,6 +1,6 @@
Info<< "Total cylinder mass: " << fvc::domainIntegrate(rho).value() << endl;
//Info<< "Total fuel mass: "
// << fvc::domainIntegrate(rho*compostion.ft()).value() << endl;
// << fvc::domainIntegrate(rho*composition.ft()).value() << endl;
OFstream logSummaryFile
(

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@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -134,7 +134,7 @@ public:
// ********************************** NB! *****************************
// for numerical reasons alpha1 and alpha2 has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha1*alpha2 when implemnting the drag
// so you MUST divide K by alpha1*alpha2 when implementing the drag
// function
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;

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@ -26,7 +26,7 @@ Class
Description
A thermal wall function for simulation of subcooled nucleate wall boiling
with runtime selctable submodels for:
with runtime selectable submodels for:
- wall heat flux partitioning model
- nucleation site density
- bubble departure frequency
@ -86,7 +86,7 @@ Usage
departureFreqModel| | yes |
\endtable
NOTE: Runtime selectabale submodels may require model specific entries
NOTE: Runtime selectable submodels may require model specific entries
Example usage:
\verbatim

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@ -29,7 +29,7 @@ Description
SourceFiles
departureDiameterModel.C
newdepartureDiameterModel.C
newDepartureDiameterModel.C
\*---------------------------------------------------------------------------*/

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@ -29,7 +29,7 @@ Description
SourceFiles
departureFrequencyModel.C
newdepartureFrequencyModel.C
newDepartureFrequencyModel.C
\*---------------------------------------------------------------------------*/

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@ -29,7 +29,7 @@ Description
SourceFiles
nucleationSiteModel.C
newnucleationSiteModel.C
newNucleationSiteModel.C
\*---------------------------------------------------------------------------*/

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@ -29,7 +29,7 @@ Description
SourceFiles
partitioningModel.C
newpartitioningModel.C
newPartitioningModel.C
\*---------------------------------------------------------------------------*/

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@ -146,7 +146,7 @@ protected:
//- Abscissa type
coordinateType coordinateType_;
//- List of volume-averaged number concentations
//- List of volume-averaged number concentrations
scalarField N_;
//- List of volume-averaged surface areas
@ -167,7 +167,7 @@ protected:
//- Highest moment order
label maxOrder_;
//- Bins (respresentative volume/area/diameter)
//- Bins (representative volume/area/diameter)
pointField bins_;
//- Bin component used according to chosen coordinate type

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@ -75,10 +75,10 @@ class nonRandomTwoLiquid
//- Name of species 2
word species2Name_;
//- Indiex of species 1 within this thermo
//- Index of species 1 within this thermo
label species1Index_;
//- Indiex of species 2 within this thermo
//- Index of species 2 within this thermo
label species2Index_;
//- Non-randomness constant parameter for species 1

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@ -71,13 +71,13 @@ class linearTsub
//- Reference diameter for low subcooling temperature
dimensionedScalar d2_;
//- Subcooling temperature where low subcooling diamter is reached
//- Subcooling temperature where low subcooling diameter is reached
dimensionedScalar Tsub2_;
//- Reference diameter for high subcooling temperature
dimensionedScalar d1_;
//- Subcooling temperature where high subcooling diamter is reached
//- Subcooling temperature where high subcooling diameter is reached
dimensionedScalar Tsub1_;
//- Diameter field

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@ -30,7 +30,6 @@ Description
SourceFiles
sinteringModel.C
newsinteringModel.C
\*---------------------------------------------------------------------------*/

View File

@ -30,7 +30,7 @@ Description
quite restrictive as it also has to support an equivalent stationary model,
which does not store motion fields or a turbulence model.
Possible future extensions include separating the turbulent fuctionality
Possible future extensions include separating the turbulent functionality
into another layer.
See also

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@ -27,7 +27,7 @@ Class
Description
Class which represents a stationary (and therefore probably solid) phase.
Generates, but does not store, zero velocity and flux field and turbulent
qauantities. Throws an error when non-const access is requested to the
quantities. Throws an error when non-const access is requested to the
motion fields or when the momentum equation is requested. Usage must
must protect against such calls.

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -64,7 +64,7 @@ void Foam::sammMesh::calcPointCells() const
// the supporting point labels, we need to work based on the cell faces.
// This is because some of the faces for meshes with arbitrary interfaces
// do not come from the cell shape, but from the slaves of the coupled
// match. It is also adventageous to remove the duplicates from the
// match. It is also advantageous to remove the duplicates from the
// point-cell addressing, because this removes a lot of waste later.
//

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@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -37,7 +37,7 @@ void Foam::sammMesh::addRegularCell
const label nCreatedCells
)
{
// Momory management
// Memory management
static labelList labelsHex(8);
static labelList labelsWedge(7);
static labelList labelsPrism(6);

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@ -27,7 +27,7 @@ Class
Description
A messy mesh class which supports the possibility of creating a shapeMesh
for regular Samm meshes (no arbitrary interfaces or collapsed SAMM cells).
If any of these special feateres exist, the mesh is created as polyMesh
If any of these special features exist, the mesh is created as polyMesh
SourceFiles
sammMesh.C

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -64,7 +64,7 @@ void Foam::starMesh::calcPointCells() const
// the supporting point labels, we need to work based on the cell faces.
// This is because some of the faces for meshes with arbitrary interfaces
// do not come from the cell shape, but from the slaves of the coupled
// match. It is also adventageous to remove the duplicates from the
// match. It is also advantageous to remove the duplicates from the
// point-cell addressing, because this removes a lot of waste later.
//

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -31,7 +31,7 @@ Description
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Specialist version of face comparison to deal with
// PROSTAR boundary format idiosyncracies
// PROSTAR boundary format idiosyncrasies
bool Foam::starMesh::starEqualFace
(
const face& boundaryFace,

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@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -993,7 +993,7 @@ void Foam::starMesh::createCoupleMatches()
// list of edges to consider. Make sure all edges are
// added such that the current point is their start.
// Loop through all edges to consider and find the one
// which produces the buggest right-hand-turn. This
// which produces the biggest right-hand-turn. This
// is the next edge to be added to the face. If its
// end is the same as the starting point, the face is
// complete; resize it to the number of active points

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -37,7 +37,7 @@ void Foam::starMesh::addRegularCell
const label nCreatedCells
)
{
// Momory management
// Memory management
static labelList labelsHex(8);
static labelList labelsPrism(6);
static labelList labelsPyramid(5);

View File

@ -27,7 +27,7 @@ Class
Description
A messy mesh class which supports the possibility of creating a shapeMesh
for regular Star meshes (no arbitrary interfaces or collapsed SAMM cells).
If any of these special feateres exist, the mesh is created as polyMesh
If any of these special features exist, the mesh is created as polyMesh
SourceFiles
calcPointCells.C

View File

@ -709,7 +709,7 @@ void countExtrudePatches
}
}
}
// Synchronise decistion. Actual numbers are not important, just make
// Synchronise decision. Actual numbers are not important, just make
// sure that they're > 0 on all processors.
Pstream::listCombineGather(zoneSidePatch, plusEqOp<label>());
Pstream::listCombineScatter(zoneSidePatch);
@ -2381,7 +2381,7 @@ int main(int argc, char *argv[])
meshMod
);
// Enforce actual point posititions according to extrudeModel (model)
// Enforce actual point positions according to extrudeModel (model)
// (extruder.setRefinement only does fixed expansionRatio)
// The regionPoints and nLayers are looped in the same way as in
// createShellMesh

View File

@ -69,8 +69,8 @@ public:
// Controls
//- Minimum cell size below which protusions through the surface are
// not split
//- Minimum cell size below which protrusions through the surface
// are not split
scalar minCellSize_;
//- Square of minCellSize
@ -114,14 +114,14 @@ public:
//- Square of span
scalar span2_;
//- Minimum edge-length of the cell size below which protusions
//- Minimum edge-length of the cell size below which protrusions
// through the surface are not split
scalar minEdgeLen_;
//- Square of minEdgeLen
scalar minEdgeLen2_;
//- Maximum notch size below which protusions into the surface are
//- Maximum notch size below which protrusions into the surface are
// not filled
scalar maxNotchLen_;

View File

@ -456,7 +456,7 @@ private:
//- Return false if the line is entirely outside the current processor
// domain, true is either point is inside, or the processor domain
// bounadry is intersected (i.e. the points are box outside but the
// boundary is intersected (i.e. the points are box outside but the
// line cuts. The points will be moved onto the box where they
// intersect.
bool clipLineToProc

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@ -636,7 +636,7 @@ bool Foam::autoDensity::fillBox
}
// Using the sampledPoints as the first test locations as they are
// randomly shuffled, but unfiormly sampling space and have wellInside
// randomly shuffled, but uniformly sampling space and have wellInside
// and size data already
maxDensity = 1/pow3(max(minCellSize, small));

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -773,7 +773,7 @@ void Foam::CV2D::newPoints()
if (!is_infinite(ec)) break;
} while (++ec != ecStart);
// Store the start-end of the first non-infinte edge
// Store the start-end of the first non-infinite edge
point2D de0 = toPoint2D(circumcenter(ec->first));
// Keep track of the maximum edge length^2

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@ -68,7 +68,7 @@ Description
randomiseInitialGrid yes;
// Perturbation fraction, 1 = cell-size.
randomPurturbation 0.1;
randomPerturbation 0.1;
// Number of relaxation iterations.
nIterations 5;

View File

@ -169,14 +169,14 @@ public:
// Friend Functions
//- Do the two given vertices consitute a boundary point-pair
//- Do the two given vertices constitute a boundary point-pair
friend bool pointPair <Gt, Vb>
(
const indexedVertex<Gt, Vb>& v0,
const indexedVertex<Gt, Vb>& v1
);
//- Do the three given vertices consitute a boundary triangle
//- Do the three given vertices constitute a boundary triangle
friend bool boundaryTriangle <Gt, Vb>
(
const indexedVertex<Gt, Vb>& v0,
@ -184,7 +184,7 @@ public:
const indexedVertex<Gt, Vb>& v2
);
//- Do the three given vertices consitute an outside triangle
//- Do the three given vertices constitute an outside triangle
friend bool outsideTriangle <Gt, Vb>
(
const indexedVertex<Gt, Vb>& v0,

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -1142,7 +1142,7 @@ void Foam::meshDualiser::setRefinement
);
}
// Detect whether different dual cells on either side of a face. This
// would neccesitate having a dual face built from the face and thus a
// would necessitate having a dual face built from the face and thus a
// dual point at the face centre.
for (label facei = 0; facei < mesh_.nInternalFaces(); facei++)
{
@ -1189,7 +1189,7 @@ void Foam::meshDualiser::setRefinement
}
// Detect whether different dual cells on either side of an edge. This
// would neccesitate having a dual face built perpendicular to the edge
// would necessitate having a dual face built perpendicular to the edge
// and thus a dual point at the mid of the edge.
// Note: not really true - the face can be built without the edge centre!
const labelListList& edgeCells = mesh_.edgeCells();

View File

@ -185,7 +185,7 @@ class vtkPVblockMesh
//- Selected curved edges
boolList edgeStatus_;
//- First instance and size of bleckMesh blocks
//- First instance and size of blockMesh blocks
// used to index into blockStatus_
arrayRange arrayRangeBlocks_;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -56,7 +56,7 @@ class tabulatedWallFunction
{
protected:
// Proteced data
// Protected data
//- Main dictionary
const dictionary dict_;

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@ -446,7 +446,7 @@ void Foam::chemkinReader::addReaction
// Calculate the unit conversion factor for the A coefficient
// for the change from mol/cm^3 to kmol/m^3 concentraction units
// for the change from mol/cm^3 to kmol/m^3 concentration units
const scalar concFactor = 0.001;
scalar sumExp = 0.0;
forAll(lhs, i)

View File

@ -118,7 +118,7 @@ surfaceConformation
// Maximum allowable protrusion through the surface before
// conformation points are added - fraction of the local target
// cell size. These small protusions are (hopefully) done by mesh filtering
// cell size. These small protrusions are (hopefully) done by mesh filtering
// instead.
maxSurfaceProtrusionCoeff 0.1;

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@ -76,7 +76,7 @@ protected:
// Protected Member Functions
//- Return the nomalized scalar error
//- Return the normalized scalar error
scalar normalizeError
(
const scalarField& y0,

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@ -55,7 +55,7 @@ class adaptiveSolver
//- Cache for dydx at the initial time
mutable scalarField dydx0_;
//- Temprorary for the test-step solution
//- Temporary for the test-step solution
mutable scalarField yTemp_;

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@ -128,7 +128,7 @@ private:
// Static data
//- Relative peturbation tolerance. Determines when point is
//- Relative perturbation tolerance. Determines when point is
// considered to be close to face/edge of bb of node.
// The tolerance is relative to the bounding box of the smallest
// node.

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -21,7 +21,7 @@ License
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
InNamspace
InNamespace
Foam
Description

View File

@ -346,7 +346,7 @@ public:
};
//- Return physical processor number (i.e. processor number in
// worldComm) given communicator and procssor
// worldComm) given communicator and processor
static int baseProcNo(const label myComm, const int procID);
//- Return processor number in communicator (given physical processor

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@ -1119,7 +1119,7 @@ Foam::label Foam::fileOperation::splitProcessorPath
if (f.size() && f[0] == 's')
{
// "processsorsNNN"
// "processorsNNN"
f = f.substr(1);

View File

@ -312,7 +312,7 @@ public:
// ) const = 0;
// (reg)IOobject functinality
// (reg)IOobject functionality
//- Generate disk file name for object. Opposite of filePath.
// Optional wanted typeName.
@ -494,7 +494,7 @@ public:
virtual void flush() const;
//- Generate path (like io.path) from root+casename with any
// 'processorXXX' replaced by procDir (usually 'processsors')
// 'processorXXX' replaced by procDir (usually 'processors')
fileName processorsCasePath
(
const IOobject&,
@ -502,7 +502,7 @@ public:
) const;
//- Generate path (like io.path) with provided instance and any
// 'processorXXX' replaced by procDir (usually 'processsors')
// 'processorXXX' replaced by procDir (usually 'processors')
fileName processorsPath
(
const IOobject&,

View File

@ -641,7 +641,7 @@ public:
// ) const;
// (reg)IOobject functinality
// (reg)IOobject functionality
//- Search for an object. checkGlobal : also check undecomposed case
virtual fileName filePath

View File

@ -108,7 +108,7 @@ Foam::fileName Foam::fileOperations::uncollatedFileOperation::filePathInfo
}
}
// Check if parallel "procesors" directory
// Check if parallel "processors" directory
if (io.time().processorCase())
{
tmpNrc<dirIndexList> pDirs

View File

@ -207,7 +207,7 @@ public:
// ) const;
// (reg)IOobject functinality
// (reg)IOobject functionality
//- Search for an object. checkGlobal : also check undecomposed case
virtual fileName filePath

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -235,7 +235,7 @@ void Foam::LduMatrix<Type, DType, LUType>::residual
// Parallel boundary initialisation.
// Note: there is a change of sign in the coupled
// interface update to add the contibution to the r.h.s.
// interface update to add the contribution to the r.h.s.
FieldField<Field, LUType> mBouCoeffs(interfacesUpper_.size());

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -89,7 +89,7 @@ void Foam::TGaussSeidelSmoother<Type, DType, LUType>::smooth
// Parallel boundary initialisation. The parallel boundary is treated
// as an effective jacobi interface in the boundary.
// Note: there is a change of sign in the coupled
// interface update to add the contibution to the r.h.s.
// interface update to add the contribution to the r.h.s.
FieldField<Field, LUType> mBouCoeffs(matrix_.interfacesUpper().size());

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -136,7 +136,7 @@ bool Foam::eagerGAMGProcAgglomeration::agglomerate()
)
);
// Use procesor agglomeration maps to do the actual
// Use processor agglomeration maps to do the actual
// collecting.
if (Pstream::myProcNo(levelComm) != -1)
{

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -183,7 +183,7 @@ bool Foam::manualGAMGProcAgglomeration::agglomerate()
)
);
// Use procesor agglomeration maps to do the actual
// Use processor agglomeration maps to do the actual
// collecting
if (Pstream::myProcNo(levelMesh.comm()) != -1)
{

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -123,7 +123,7 @@ bool Foam::masterCoarsestGAMGProcAgglomeration::agglomerate()
)
);
// Use procesor agglomeration maps to do the actual collecting.
// Use processor agglomeration maps to do the actual collecting.
if (Pstream::myProcNo(levelComm) != -1)
{
GAMGProcAgglomeration::agglomerate

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -303,7 +303,7 @@ bool Foam::procFacesGAMGProcAgglomeration::agglomerate()
);
// Use procesor agglomeration maps to do the actual
// Use processor agglomeration maps to do the actual
// collecting.
GAMGProcAgglomeration::agglomerate
(

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2013-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2013-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -384,7 +384,7 @@ Foam::lduPrimitiveMesh::lduPrimitiveMesh
const lduInterfacePtrsList interfaces =
mesh(myMesh, otherMeshes, procMeshI).interfaces();
// Inialise all boundaries as merged
// Initialise all boundaries as merged
boundaryMap[procMeshI].setSize(interfaces.size(), -1);
boundaryFaceMap[procMeshI].setSize(interfaces.size());

View File

@ -135,7 +135,7 @@ public:
//- Return interpolated addressing
virtual const labelListList& addressing() const;
//- Return interpolaion weights
//- Return interpolation weights
virtual const scalarListList& weights() const;
//- Are there any inserted points

View File

@ -143,7 +143,7 @@ public:
//- Return interpolated addressing
virtual const labelListList& addressing() const;
//- Return interpolaion weights
//- Return interpolation weights
virtual const scalarListList& weights() const;

View File

@ -134,7 +134,7 @@ public:
//- Return interpolated addressing
virtual const labelListList& addressing() const;
//- Return interpolaion weights
//- Return interpolation weights
virtual const scalarListList& weights() const;
//- Are there any inserted cells

View File

@ -138,7 +138,7 @@ public:
//- Return interpolated addressing
virtual const labelListList& addressing() const;
//- Return interpolaion weights
//- Return interpolation weights
virtual const scalarListList& weights() const;
//- Return flux flip map

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -148,7 +148,7 @@ Foam::vector Foam::eigenVector
scalar sd0, sd1, sd2;
scalar magSd0, magSd1, magSd2;
// Sub-determinants for a unique eivenvalue
// Sub-determinants for a unique eigenvalue
sd0 = A.yy()*A.zz() - A.yz()*A.zy();
sd1 = A.zz()*A.xx() - A.zx()*A.xz();
sd2 = A.xx()*A.yy() - A.xy()*A.yx();

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -21,7 +21,7 @@ License
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
InNamspace
InNamespace
Foam
Description

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2012-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2012-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -21,7 +21,7 @@ License
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
InNamspace
InNamespace
Foam
Description

View File

@ -38,7 +38,7 @@ Description
<magSfN> <valueN> <qDotN> <htcN>
\endverbatim
and received as the constituent pieces of the `mixed' condition, i.e.
and received as the constitutent pieces of the `mixed' condition, i.e.
\verbatim
# Patch: <patch name>

View File

@ -38,8 +38,8 @@ Description
where
\vartable
\alpha_t| turblence thermal diffusivity
\mu_t | turblence viscosity
\alpha_t| turbulence thermal diffusivity
\mu_t | turbulence viscosity
Pr_t | turblent Prandtl number
\endvartable

View File

@ -35,8 +35,8 @@ Description
where
\vartable
epsilon | turblence dissipation field
G | turblence generation field
epsilon | turbulence dissipation field
G | turbulence generation field
\endvartable
The model switches between laminar and turbulent functions based on the

View File

@ -38,7 +38,7 @@ Description
pc is considered from the IFC solution.
omegaFuelBar is calculated solving a relaxation equation which tends to
omegaEq. This omegaEq is obtained from the flamelet solution for
different strain rates and fit using a expential distribution.
different strain rates and fit using a exponential distribution.
The spacial distribution of the consumption speed (omega) is obtained also
from a strained flamelet solution and it is assumed to have a gaussian
@ -93,7 +93,7 @@ class FSD
//- Fuel mass concentration on the fuel stream
dimensionedScalar YFuelFuelStream_;
//- Oxygen mass concentration on the oxydizer stream
//- Oxygen mass concentration on the oxidizer stream
dimensionedScalar YO2OxiStream_;
//- Similarity constant for the sub-grid ft fluctuations

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -624,7 +624,7 @@ Body:
where boundaryType is truncated to 4 characters from one of the following:
INLET
PRESSSURE
PRESSURE
OUTLET
BAFFLE
etc,

View File

@ -848,7 +848,7 @@ void Foam::boundaryMesh::writeTriSurface(const fileName& fName) const
// Get index in this (boundaryMesh) of face nearest to each boundary face in
// pMesh.
// Origininally all triangles/faces of boundaryMesh would be bunged into
// Originally all triangles/faces of boundaryMesh would be bunged into
// one big octree. Problem was that faces on top of each other, differing
// only in sign of normal, could not be found separately. It would always
// find only one. We could detect that it was probably finding the wrong one

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -520,7 +520,7 @@ Foam::multiDirRefinement::multiDirRefinement
}
// Construct from directionary and directions to refine.
// Construct from dictionary and directions to refine.
Foam::multiDirRefinement::multiDirRefinement
(
polyMesh& mesh,

View File

@ -255,7 +255,7 @@ Foam::displacementLayeredMotionMotionSolver::faceZoneEvaluate
}
else if (type == "uniformFollow")
{
// Reads name of name of patch. Then get average point dislacement on
// Reads name of name of patch. Then get average point displacement on
// patch. That becomes the value of fld.
const word patchName(dict.lookup("patch"));
label patchID = mesh().boundaryMesh().findPatchID(patchName);

View File

@ -67,7 +67,7 @@ class rotatingMotion
//- Axis vector
const vector axis_;
//- Angular velocty (rad/sec)
//- Angular velocity (rad/sec)
autoPtr<Function1<scalar>> omega_;

View File

@ -247,7 +247,7 @@ public:
return owner_;
}
//- Return neighour cell
//- Return neighbour cell
label neighbour() const
{
return neighbour_;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -104,7 +104,7 @@ void Foam::duplicatePoints::setRefinement
// Modfify faces according to face region
// Modify faces according to face region
// ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
face newFace;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2012-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2012-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -449,7 +449,7 @@ void Foam::tetDecomposer::setRefinement
label nextFp = f.fcIndex(fp);
// Triangle triI consisiting of f[fp0], f[fp], f[nextFp]
// Triangle triI consisting of f[fp0], f[fp], f[nextFp]
// 1. Front triangle (decomposition of face itself)

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -384,7 +384,7 @@ void Foam::slidingInterface::coupleInterface(polyTopoChange& ref) const
// cutPointEdgePairMap
// Note. "Processing slave edges" code is repeated twice in the
// sliding intergace coupling in order to allow the point
// sliding interface coupling in order to allow the point
// projection to be done separately from the actual cutting.
// Please change consistently with slidingInterfaceProjectPoints.C
//

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -729,7 +729,7 @@ bool Foam::slidingInterface::projectPoints() const
scalarField masterPointEdgeDist(masterLocalPoints.size(), great);
// Note. "Processing slave edges" code is repeated twice in the
// sliding intergace coupling in order to allow the point
// sliding interface coupling in order to allow the point
// projection to be done separately from the actual cutting.
// Please change consistently with coupleSlidingInterface.C
//

View File

@ -104,7 +104,7 @@ class MRFZone
//- Axis vector
vector axis_;
//- Angular velocty (rad/sec)
//- Angular velocity (rad/sec)
autoPtr<Function1<scalar>> omega_;

View File

@ -81,7 +81,7 @@ protected:
//- Axis of rotation, a direction vector which passes through the origin
vector axis_;
//- SRF model coeficients dictionary
//- SRF model coefficients dictionary
dictionary SRFModelCoeffs_;
//- Angular velocity of the frame (rad/s)

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2011-2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -76,7 +76,7 @@ bool Foam::setRefCell
label sumHasRef = returnReduce<label>(hasRef, sumOp<label>());
// If reference cell no found use octree search
// with cell tet-decompositoin
// with cell tet-decomposition
if (sumHasRef != 1)
{
refCelli = field.mesh().findCell(refPointi);

View File

@ -153,10 +153,10 @@ public:
//- Return true if all convergence checks are satisfied
virtual bool criteriaSatisfied() const = 0;
//- Flag to indicate whether convergance has been reached
//- Flag to indicate whether convergence has been reached
bool converged();
//- End the run if convergance has been reached
//- End the run if convergence has been reached
bool endIfConverged(Time& time);

View File

@ -72,8 +72,8 @@ protected:
// than PISO mode
bool simpleRho_;
//- Flag to control whether turblence is solved just on the final pimple
// iteration, or on every pimple iteration
//- Flag to control whether turbulence is solved just on the final
// pimple iteration, or on every pimple iteration
bool turbOnFinalIterOnly_;

View File

@ -25,7 +25,7 @@ Class
Foam::calculatedFvPatchField
Description
This boundary condition is not designed to be evaluated; it is assmued
This boundary condition is not designed to be evaluated; it is assumed
that the value is assigned via field assignment, and not via a call to
e.g. \c updateCoeffs or \c evaluate.

View File

@ -40,7 +40,7 @@ Usage
Note
The outer boundary of the patch pairs must be similar, i.e. if the owner
patch is transformed to the neighbour patch, the outer perimiter of each
patch is transformed to the neighbour patch, the outer perimeter of each
patch should be identical (or very similar).
See also

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Copyright (C) 2018 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2018-2019 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -40,7 +40,7 @@ Usage
Note
The outer boundary of the patch pairs must be similar, i.e. if the owner
patch is transformed to the neighbour patch, the outer perimiter of each
patch is transformed to the neighbour patch, the outer perimeter of each
patch should be identical (or very similar).
See also

View File

@ -35,7 +35,7 @@ Usage
Property | Description | Required | Default value
phi | flux field name | no | phi
tangentialVelocity | tangential velocity field | no |
omega | angular velocty of the frame [rad/s] | yes |
omega | angular velocity of the frame [rad/s] | yes |
\endtable
Example of the boundary condition specification:

View File

@ -37,7 +37,7 @@ Usage
psi | compressibility field name | no | none
gamma | ratio of specific heats (Cp/Cv) | yes |
p0 | static pressure reference | yes |
omega | angular velocty of the frame [rad/s] | yes |
omega | angular velocity of the frame [rad/s] | yes |
\endtable
Example of the boundary condition specification:

View File

@ -32,7 +32,7 @@ Usage
Property | Description | Required | Default value
origin | origin of rotation in Cartesian co-ordinates | yes|
axis | axis of rotation | yes |
omega | angular velocty of the frame [rad/s] | yes |
omega | angular velocity of the frame [rad/s] | yes |
\endtable
Example of the boundary condition specification:

View File

@ -26,7 +26,7 @@ Class
Description
This boundary condition provides a velocity boundary condition for
multphase flow based on a user-specified volumetric flow rate.
multiphase flow based on a user-specified volumetric flow rate.
The flow rate is made proportional to the phase fraction alpha at each
face of the patch and alpha is ensured to be bound between 0 and 1.

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