Flunt帮助算例总结Word文档格式.docx
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Preparation
1.Copythefileelbow/elbow.mshfromtheFLUENTdocumentationCDtoyourworkingdirectory.
ForUNIXsystems,youcanfindthefilebyinsertingtheCDintoyourCD-ROMdriveandgoingtothefollowingdirectory:
/cdrom/fluent6.0/help/tutfiles/
wherecdrommustbereplacedbythenameofyourCD-ROMdrive.
ForWindowssystems,youcanfindthefilebyinsertingtheCDintoyourCD-ROMdriveandgoingtothefollowingdirectory:
cdrom:
\fluent6.0\help\tutfiles\
wherecdrommustbereplacedbythenameofyourCD-ROMdrive(e.g.,E).
2.Startthe2DversionofFLUENT.
2.ModelingPeriodicFlowandHeatTransfer
ProblemDescription
Thisproblemconsidersa2Dsectionofatubebank.AschematicoftheproblemisshowninFigure
2.1.Thebankconsistsofuniformlyspacedtubeswithadiameterof1cm,thatarestaggeredinthedirectionofcross-fluidflow.Theircentersareseparatedbyadistanceof2cminthexdirection,and1cmintheydirection.Thebankhasadepthof1m.
Becauseofthesymmetryofthetubebankgeometry,onlyaportionofthedomainneedstobemodeled.ThecomputationaldomainisshowninoutlineinFigure
2.1.Amassflowrateof0.05kg/sisappliedtotheinflowboundaryoftheperiodicmodule.Thetemperatureofthetubewall(
)is400Kandthebulktemperatureofthecross-flowwater(
)is300K.ThepropertiesofwaterthatareusedinthemodelareshowninFigure
2.1.
Figure2.1:
SchematicoftheProblem
1.
Copythefiletubebank/tubebank.mshfromtheFLUENTdocumentationCDtoyourworkingdirectory(asdescribedinTutorial
1).
2.
Startthe2DversionofFLUENT.
3.ModelingExternalCompressibleFlow
Theproblemconsiderstheflowaroundanairfoilatanincidenceangleof
andafreestreamMachnumberof0.8(
).Thisflowistransonic,andhasafairlystrongshocknearthemid-chord(x/c=0.45)ontheupper(suction)side.Thechordlengthis1m.ThegeometryoftheairfoilisshowninFigure
3.1.
Figure3.1:
Copythefileairfoil/airfoil.mshfromtheFLUENTdocumentationCDtoyourworkingdirectory(asdescribedinTutorial
Startthe2DversionofFLUENT.
4.ModelingUnsteadyCompressibleFlow
5.ModelingRadiationandNaturalConvection
6.UsingaNon-ConformalMesh
Thisproblemconsidersamodelofa3Dsectionofafilmcoolingtestrig.AschematicisshowninFigures
6.1and6.2.Theproblemconsistsofaduct,24.5inlong,withcross-sectionaldimensionsof0.75in
5in.Anarrayofuniformlyspacedholesislocatedatthebottomoftheduct.Eachholehasadiameterof0.5inches,isinclinedat35degrees,andisspaced1.5inchesapartlaterally.Coolerinjectedairentersthesystemthroughtheplenum,withcross-sectionaldimensionsof3.3in
1.25in.
Becauseofthesymmetryofthegeometry,onlyaportionofthedomainneedstobemodeled.ThecomputationaldomainisshowninoutlineinFigure
6.2.Thebulktemperatureofthestreamwiseair(
)is273K,andthevelocityoftheairstreamis20m/s.Thebottomwalloftheductthatintersectstheholearrayisassumedtobeacompletelyinsulated(adiabatic)wall.Thesecondary(injected)airenterstheplenumatauniformvelocityof0.4559m/s.Thetemperatureoftheinjectedair(
)is136.6
K.ThepropertiesofairthatareusedinthemodelareshowninFigure
6.2.
Figure6.1:
SchematicoftheProblem,FrontView
Figure6.2:
SchematicoftheProblem,TopView
Copythefilesfilmcool/film_hex.mshandfilmcool/film_tet.mshfromtheFLUENTdocumentationCDtoyourworkingdirectory(asdescribedinTutorial
Step1:
MergingtheMeshFiles
Startthe3Dversionoftmergebytypingutilitytmerge-3datthesystemprompt.
Providethemeshfilenamesfilm_tet.mshandfilm_hex.mshasprompted.Providescalingof1andtranslationsandrotationsofzeroforeachmeshfile.Savethenewmergedmeshfileasfilmcool.msh.
Append3Dgridfiles.
tmerge3DFluentInc,Version2.1.8
Enternameofgridfile(ENTERtocontinue):
film_tet.msh
x,y,zscalingfactor,eg.111:
111
x,y,ztranslation,eg.010:
000
rotaxis(0,1,2),angle(deg),eg.145:
00
film_hex.msh
<
ENTER>
Enternameofoutputfile:
filmcool.msh
!
Themeshfilesmustbereadintotmergeinthisorderforthetutorialtorunaswritten.Otherwise,zonenamesandnumberswillbeassigneddifferentlywhenthefilesaremergedtogether.Ingeneral,however,youcanspecifyfilestobereadintotmergeinanyorder.
7.UsingaSingleRotatingReferenceFrame
8.UsingMultipleRotatingReferenceFrames
9.UsingtheMixingPlaneModel
10.UsingSlidingMeshes
11.ModelingSpeciesTransportandGaseousCombustion
12.UsingtheNon-PremixedCombustionModel
13.ModelingSurfaceChemistry
14.ModelingEvaporatingLiquidSpray
15.UsingtheVOFModel
16.ModelingCavitation
17.UsingtheMixtureandEulerianMultiphaseModels
18.UsingtheEulerianMultiphaseModelforGranularFlow
19.ModelingSolidification
20.Postprocessing
21.TurboPostprocessing
22.ParallelProcessing