Difference between revisions of "OpenFOAM/C2/2D-Laminar-Flow-in-a-channel/English"
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− | Keywords: Video tutorial,CFD,laminar flow,simpleFoam,channel | + | Keywords: Video tutorial,CFD,laminar flow,simpleFoam,channel |
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| style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 1 | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 1 | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Hello and welcome to the spoken tutorial on Simulating Laminar Flow in a Channel using openfoam | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Hello and welcome to the spoken tutorial on '''Simulating 2D Laminar Flow in a Channel using openfoam''' |
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| style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In this tutorial I will show you | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In this tutorial I will show you | ||
+ | *'''2D geometry of channel ''' | ||
+ | *'''Meshing the Geometry''' | ||
+ | *'''Solving''' and '''Post Processing results''' in '''Paraview''' | ||
+ | *and Validation using '''analytic result''' | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 3 : System requirement | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| To record this tutorial I am using | ||
+ | * '''Linux Operating system Ubuntu 12.04''' . | ||
+ | *'''OpenFOAM version 2.1.1''' | ||
+ | *'''ParaView version 3.12.0 ''' | ||
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+ | Note that '''OpenFOAM''' version '''2.1.1''' is supported on '''Ubuntu version 12.04''' | ||
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− | + | Hence forth all the tutorials will be covered using '''OpenFOAM version 2.1.1''' and''' Ubuntu version 12.04''' | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 4 : System Requirement |
+ | * The tutorials were recorded using the versions specified in previous slide | ||
− | + | * Subsequently the tutorials were edited to latest versions | |
− | + | ||
+ | * To install latest system requirements go to Installation Sheet | ||
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 5 : Prerequisite | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| As a prerequisite for this tutorial, you should know how to create '''geometry''' using '''OpenFOAM.''' | ||
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+ | If not, please refer to the relevant tutorials on our website. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 6 : About flow in a channel | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | ||
+ | We '''simulate flow''' in a '''Channel''' to determine '''Flow development length''' along the downstream. | ||
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− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 7 : Channel Flow | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''Channel flow''' problem description. | |
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− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 7 : Channel flow | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''boundary names''' and '''inlet conditions''' are shown in this figure. | ||
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 8 : Boundary Conditions |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''flow develpoment length''' is given by the formula |
− | + | '''L = 0.05 * Re * D''' | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 8 : Boundary Conditions |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''Re''' which is the '''Reynolds number''' |
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+ | and '''D''' which is the '''channel height''' | ||
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 8 : Boundary Conditions |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Using the '''formula''' the '''length''' of the '''channel''' comes out to be '''5 meters ''' |
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− | + | and '''height''' is kept as '''1 meters'''. | |
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+ | The '''Inlet velocity is 1''' '''meters per second''' | ||
+ | And we are solving this for a '''Reynolds number ( Re ) equal 100''' | ||
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 9 : File structure |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| This is a steady state problem | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| This is a '''steady state problem ''' |
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+ | *Therefore we are using a '''steady state incompressible''' solver for this '''case'''. | ||
+ | *This is the '''file structure''' of our '''case'''. | ||
+ | *The '''folder''' should be created in the '''solver type''' that we choose. | ||
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Create a '''folder''' and name it as channel in '''simpleFoam folder'''. |
− | + | right click >> new folder | |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| I have already created a '''folder''' in |
− | + | '''simpleFoam folder''' of''' incompressible flow solvers'''. | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Nmae the folder channel |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''folder''' is named as''' channel'''. | ||
− | + | Now let me switch to the '''folder'''. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| copy 0,constant and system from pitzDaily to this channel folder | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Copy '''0, Constant''' and '''System folders''' of any other '''case'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In the '''simpleFoam directory''', I have copied the''' file structure''' of '''case''' of''' pitzDaily'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Paste it in the '''channel folder'''. | ||
− | + | And make the necessary changes in the '''geometry, boundary faces''' and '''boundary condition'''. | |
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− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now let me open the '''command terminal'''. | |
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| style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Press Ctrl+Alt+t keys simultaneously | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Press Ctrl+Alt+t keys simultaneously | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| To do this press '''Ctrl+Alt +t''' keys simultaneously on your '''keyboard'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| run and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In the '''terminal''', type '''run''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''cd space tutorials''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| incompressible and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''cd space incompressible''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| simpleFoam and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Type '''cd space simpleFoam''' and press '''Enter'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| channel and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''cd space channel''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| ls and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''ls''' and press '''Enter'''. | ||
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− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| You will see three '''folders 0 , Constant and System''' | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | |
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cd constant and press enter | cd constant and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''cd space constant''' and press '''Enter'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| ls and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''ls''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| polymesh folder and 2 other files | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In this you will see '''files''' containing '''properties of fluid''' and a''' folder''' named '''polymesh'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| gedit RASProperties and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''RASProperties''' contains '''Reynolds-averaged stress model'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Transportproperties | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''transportProperties''' contain the '''transport model'''. | ||
− | + | And '''kinematic viscosity''' (that is '''nu'''), in this '''case''', is set at '''0.001 m²/s (meter square per second)'''. | |
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| cd polyMesh and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now in the '''terminal''' type '''cd polyMesh''' and press '''Enter'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| ls and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now type '''ls''' and press '''Enter'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| You will see the '''blockMeshDict''' file here. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| gedit blockMeshDict and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| To open the '''blockMeshDict''' file in the '''terminal '''type '''gedit blockMeshDict and press '''Enter'''. | ||
− | + | Scroll down. | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right: | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In the blockMeshDict file covertTometers is set to 1 |
− | + | Set the vertices for channel | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''geometry''' is in '''meters '''so the '''convertTometers''' is set to 1. | ||
− | + | Next we have defined the '''vertices of the channel'''. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Mesh size for channel | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| We have used a '''100 X 100 mesh size''' here and '''cell spacing''' is kept as '''( 1 1 1 )'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Boundary conditions and types | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Next we have set up '''boundary conditions''' and their '''types''' which are '''inlet ,outlet,top''' and '''bottom'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| FrontAndBack boundary type as empty | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| As this is a '''2D geometry, frontAndBack''' is kept as '''empty'''. | ||
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+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Due to a 2 dimensional geometry | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Also this being a '''simple geometry, mergePatchPair''' and '''edges''' are to be kept '''empty'''. | ||
− | + | Close the '''blockMeshDict''' file. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Terminal window | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In the '''command terminal''' type '''cd space ..(dot dot) '''and press '''Enter'''. | ||
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− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Terminal window | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Again type '''cd space .. (dot dot)''' and press '''Enter'''. | |
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− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In the '''terminal''' type '''cd 0''' |
− | + | ||
− | + | ||
− | + | ||
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− | In terminal type | + | |
− | + | ||
− | cd | + | |
type ls and press enter | type ls and press enter | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now in the '''terminal''' type '''cd space 0 (Zero)''' and press '''Enter'''. |
− | + | Now type''' ls''' and press '''Enter'''. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In terminal you can see these slides | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| This contains the '''initial boundary conditions ''' and''' wall functions''' for the '''channel case'''. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Wall functions : epsilon, k, nut, nutilda | ||
− | + | initial flow conditions: p, R and U | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| It should contain various files such as '''epsilon ,k, nut,nuTilda ''' which are the '''wall functions'''. | ||
− | |||
+ | And '''p , R''' and capital '''U''' which the are '''initial conditions of the flow'''. | ||
− | + | Now let me switch back to the slides. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 10 : Calculate K. | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''Calculate k''' which is the '''turbulent kinetic energy''' from the formula given in the slide. | ||
− | |||
+ | Where '''Ux, Uy and Uz''' are the '''velocity''' components in the '''x, y''' and '''z direction'''. | ||
− | |||
− | + | And '''U' ( dash ) = 0.05''' times '''u''' actual. | |
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|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 11 : Calculate epsilon |
− | + | epsilon - rate of disspiation turbulent kinetic energy | |
− | + | C mu - constant | |
− | |||
+ | l – length of channel | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Calculate '''epsilon''' from the '''formula''' given: | ||
− | |||
− | + | Where '''epsilon''' is the''' rate of disspiation turbulent kinetic energy'''. | |
− | + | ||
− | + | '''C mu''' is a '''constant''' and its value is''' 0.09''' | |
− | + | And''' l''' is the '''length of the channel'''. | |
− | + | Let me minimise this. | |
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Change only the boundary names | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Change only the '''boundary names''' in each of the above files. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Do not chnge the values of nu,nuTilde and R | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Note that the values of '''nut, nuTilda''' and '''R ''' are kept to be default. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Rest of the files should contain '''initial value''' for each of the '''boundary faces'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In the terminal window type '''cd ..''' and press enter | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now in the '''terminal''' type '''cd (space) ..(dot dot)''' and press '''Enter'''. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| No change in system folder | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| There are no changes to be done in the '''system folder'''. | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Mesh the geometry | ||
− | |||
+ | terminal window type : blockMesh | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now, we need to '''mesh the geometry'''. | ||
− | |||
+ | To do this, in the '''command terminal''' type '''blockMesh''' and press '''Enter'''. | ||
− | |||
+ | The '''Meshing''' is done. | ||
− | |||
+ | Let me switch back to the slide. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 12 : Solver | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''type of solver''' we are using here is '''simpleFoam'''. | ||
− | + | It is a '''Steady-state solver''' for '''incompressible''' and '''turbulent flows'''. | |
− | + | Let me minimise this. | |
− | + | |- | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Type simpleFoam and press enter | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In the '''command terminal''' type '''simpleFoam''' and press '''Enter'''. | |
− | + | ||
− | + | ||
− | + | ||
− | + | ||
− | + | ||
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Iterations in terminal window |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''Iterations''' running will be seen in the '''command terminal'''. |
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| '''Iterations '''running may take some time. |
− | + | ||
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Iterations converge or stop at end of time step |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The '''iterations''' will stop once the '''solution''' is '''converged''' or it reaches its '''end time value'''. | |
− | + | ||
− | + | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | |
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|- | |- | ||
Line 387: | Line 379: | ||
type: paraFoam and press enter | type: paraFoam and press enter | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| To view the results in | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| To view the results in '''ParaView''' in the '''terminal,''' type '''paraFoam and press '''Enter'''. |
− | + | This will open up the '''ParaView''' window. | |
− | + | ||
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In paraview window |
− | + | View the geometry | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| On left hand side of the '''ParaView''' window click '''Apply'''. | ||
− | + | The '''geometry '''can be seen here. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Change from solid color to U | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| On top of '''active variable control menu''' change the drop-down menu from '''solid color''' to capital '''U'''. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Look at left side of the channel geometry | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| You can see the '''initial state''' of '''velocity magnitude''' at '''inlet.''' | ||
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| VCR control click PLAY button | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| On top of the '''ParaView''' window, click on the '''play''' button of the '''VCR control'''. | ||
− | |||
+ | You can see the final value of the '''velocity magnitude'''. | ||
− | + | |- | |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Color legend from top left |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Also toggle on the '''color legend''' from the left hand side top of the '''active variable control menu'''. | ||
− | + | Click '''Apply''' again. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| In object inspector menu | ||
− | |||
+ | click on rescale to data | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Now go to '''Display'''. | ||
− | |||
+ | Scroll down. You can see '''Rescale''', click on it. | ||
− | + | |- | |
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Check the color legend for this | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| We can see that once the '''flow''' has fully developed, it attains a '''maximum uniform velocity''' at the '''center'''. | ||
− | + | Now let me switch back to the slides. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 13 :Validation | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The results obtained can be '''validated '''with the '''analytical solution''' for '''laminar flow''' in a | ||
+ | '''channel''' which is '''u(max)=1.5 Uavg''' | ||
− | |||
+ | Using '''OpenFOAM''' we obtain a result of '''u(max)''' equal to '''1.48 meters per second''' which is a good match. | ||
+ | This brings us to the end of the tutorial. | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 14 : Summary |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| In this tutorial we learnt |
+ | |||
+ | *The '''file structure of channel''' | ||
+ | *Obtained '''solution''' using '''steady state solver''' | ||
+ | *Viewed the '''geometry''' in '''ParaView ''' | ||
+ | *'''Validation''' with '''analytic results''' | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 15 : |
− | + | ||
+ | Assignment | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| As an assignment: | ||
− | + | *Solve the problem for '''Reynold Number 1500''' and | |
+ | *'''Validate''' it with the '''analytical result''' | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 16 : About the Spoken Tutorial Project |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| Watch the video available at this URL. |
+ | It summarizes the Spoken Tutorial project. | ||
− | + | If you do not have good bandwidth, you can download and watch it. | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 17 : Spoken Tutorial Workshops | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| The Spoken Tutorial Project Team | ||
− | + | -Conducts workshops using spoken tutorials | |
+ | -Gives certificates to those who pass an online test | ||
− | + | -For more details, please write to [mailto:contact@spoken-tutorial.org contact@spoken-tutorial.org] | |
+ | |- | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 18 : | ||
− | + | Forum to answer questions | |
+ | * Do you have questions on THIS Spoken Tutorial? | ||
+ | * Choose the minute and second where you have the question | ||
+ | * Explain your question briefly | ||
+ | * Someone from the FOSSEE team will answer them. Please visit | ||
+ | http://forums.spoken-tutorial.org/ | ||
+ | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 19: |
− | + | Forum to answer questions | |
− | + | * Questions not related to the Spoken Tutorial? | |
− | + | * Do you have general/technical questions on the Software? | |
− | + | * Please visit the FOSSEE forum | |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | http://forums.fossee.in/ |
− | + | * Choose the Software and post your question | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | |
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 20: |
− | + | Lab Migration Project | |
− | + | * We coordinate migration from commercial CFD software like ANSYS to OpenFOAM | |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | * We conduct free Workshops and provide solutions to CFD Problem Statements in OpenFOAM |
− | + | For more details visit this site: | |
− | + | http://cfd.fossee.in/ | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | |
− | + | ||
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 21: |
− | + | Case Study Project | |
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | + | * We invite students to solve a feasible CFD problem statement of reasonable complexity using OpenFOAM |
− | + | * We give honorarium and certificate to those who do this | |
− | + | For more details visit this site: | |
− | + | http://cfd.fossee.in/ | |
− | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| | |
− | + | ||
− | + | ||
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| Slide 22: |
Acknowledgement | Acknowledgement | ||
− | |||
Line 511: | Line 532: | ||
It is supported by the National Mission on Education through ICT, MHRD, Government of India. | It is supported by the National Mission on Education through ICT, MHRD, Government of India. | ||
− | + | More information on the same is available at the following URL http://spoken-tutorial.org/NMEICT-Intro | |
− | + | ||
− | More information on the same is available at the following URL | + | |
|- | |- | ||
− | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| | + | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:none;padding:0.097cm;"| About the contributor |
− | + | ||
− | About the contributor | + | |
| style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| This is Rahul Joshi from IIT BOMBAY signing off. | | style="border-top:none;border-bottom:0.05pt solid #000000;border-left:0.05pt solid #000000;border-right:0.05pt solid #000000;padding:0.097cm;"| This is Rahul Joshi from IIT BOMBAY signing off. | ||
− | Thanks for joining | + | Thanks for joining |
|} | |} |
Latest revision as of 07:44, 13 June 2019
Tutorial: Simulating Laminar flow in a channel.
Script and Narration : Rahul Joshi
Keywords: Video tutorial,CFD,laminar flow,simpleFoam,channel
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Slide 1 | Hello and welcome to the spoken tutorial on Simulating 2D Laminar Flow in a Channel using openfoam |
Slide 2 : Learning Objectives | In this tutorial I will show you
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Slide 3 : System requirement | To record this tutorial I am using
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Slide 4 : System Requirement
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Slide 5 : Prerequisite | As a prerequisite for this tutorial, you should know how to create geometry using OpenFOAM.
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Slide 6 : About flow in a channel |
We simulate flow in a Channel to determine Flow development length along the downstream. |
Slide 7 : Channel Flow | Channel flow problem description. |
Slide 7 : Channel flow | The boundary names and inlet conditions are shown in this figure. |
Slide 8 : Boundary Conditions | The flow develpoment length is given by the formula
L = 0.05 * Re * D |
Slide 8 : Boundary Conditions | Re which is the Reynolds number
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Slide 8 : Boundary Conditions | Using the formula the length of the channel comes out to be 5 meters
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Slide 9 : File structure | This is a steady state problem
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Create a folder and name it as channel in simpleFoam folder.
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I have already created a folder in
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Nmae the folder channel | The folder is named as channel.
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copy 0,constant and system from pitzDaily to this channel folder | Copy 0, Constant and System folders of any other case. |
In the simpleFoam directory, I have copied the file structure of case of pitzDaily. | |
Paste it in the channel folder.
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Now let me open the command terminal. | |
Press Ctrl+Alt+t keys simultaneously | To do this press Ctrl+Alt +t keys simultaneously on your keyboard. |
run and press enter | In the terminal, type run and press Enter. |
Now type cd space tutorials and press Enter. | |
incompressible and press enter | Now type cd space incompressible and press Enter. |
simpleFoam and press enter | Type cd space simpleFoam and press Enter. |
channel and press enter | Now type cd space channel and press Enter. |
ls and press enter | Now type ls and press Enter. |
You will see three folders 0 , Constant and System | |
Type in command terminal
cd constant and press enter |
Now type cd space constant and press Enter. |
ls and press enter | Now type ls and press Enter. |
polymesh folder and 2 other files | In this you will see files containing properties of fluid and a folder named polymesh. |
gedit RASProperties and press enter | RASProperties contains Reynolds-averaged stress model. |
Transportproperties | transportProperties contain the transport model.
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cd polyMesh and press enter | Now in the terminal type cd polyMesh and press Enter. |
ls and press enter | Now type ls and press Enter. |
You will see the blockMeshDict file here. | |
gedit blockMeshDict and press enter | To open the blockMeshDict file in the terminal type gedit blockMeshDict and press Enter.
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In the blockMeshDict file covertTometers is set to 1
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The geometry is in meters so the convertTometers is set to 1.
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Mesh size for channel | We have used a 100 X 100 mesh size here and cell spacing is kept as ( 1 1 1 ). |
Boundary conditions and types | Next we have set up boundary conditions and their types which are inlet ,outlet,top and bottom. |
FrontAndBack boundary type as empty | As this is a 2D geometry, frontAndBack is kept as empty. |
Due to a 2 dimensional geometry | Also this being a simple geometry, mergePatchPair and edges are to be kept empty.
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Terminal window | In the command terminal type cd space ..(dot dot) and press Enter. |
Terminal window | Again type cd space .. (dot dot) and press Enter. |
In the terminal type cd 0
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Now in the terminal type cd space 0 (Zero) and press Enter.
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In terminal you can see these slides | This contains the initial boundary conditions and wall functions for the channel case. |
Wall functions : epsilon, k, nut, nutilda
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It should contain various files such as epsilon ,k, nut,nuTilda which are the wall functions.
Now let me switch back to the slides. |
Slide 10 : Calculate K. | Calculate k which is the turbulent kinetic energy from the formula given in the slide.
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Slide 11 : Calculate epsilon
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Calculate epsilon from the formula given:
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Change only the boundary names | Change only the boundary names in each of the above files. |
Do not chnge the values of nu,nuTilde and R | Note that the values of nut, nuTilda and R are kept to be default. |
Rest of the files should contain initial value for each of the boundary faces. | |
In the terminal window type cd .. and press enter | Now in the terminal type cd (space) ..(dot dot) and press Enter. |
No change in system folder | There are no changes to be done in the system folder. |
Mesh the geometry
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Now, we need to mesh the geometry.
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Slide 12 : Solver | The type of solver we are using here is simpleFoam.
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Type simpleFoam and press enter | In the command terminal type simpleFoam and press Enter. |
Iterations in terminal window | Iterations running will be seen in the command terminal. |
Iterations running may take some time. | |
Iterations converge or stop at end of time step | The iterations will stop once the solution is converged or it reaches its end time value. |
In terminal
type: paraFoam and press enter |
To view the results in ParaView in the terminal, type paraFoam and press Enter.
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In paraview window
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On left hand side of the ParaView window click Apply.
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Change from solid color to U | On top of active variable control menu change the drop-down menu from solid color to capital U. |
Look at left side of the channel geometry | You can see the initial state of velocity magnitude at inlet. |
VCR control click PLAY button | On top of the ParaView window, click on the play button of the VCR control.
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Color legend from top left | Also toggle on the color legend from the left hand side top of the active variable control menu.
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In object inspector menu
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Now go to Display.
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Check the color legend for this | We can see that once the flow has fully developed, it attains a maximum uniform velocity at the center.
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Slide 13 :Validation | The results obtained can be validated with the analytical solution for laminar flow in a
channel which is u(max)=1.5 Uavg
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Slide 14 : Summary | In this tutorial we learnt
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Slide 15 :
Assignment |
As an assignment:
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Slide 16 : About the Spoken Tutorial Project | Watch the video available at this URL.
It summarizes the Spoken Tutorial project. If you do not have good bandwidth, you can download and watch it. |
Slide 17 : Spoken Tutorial Workshops | The Spoken Tutorial Project Team
-Conducts workshops using spoken tutorials -Gives certificates to those who pass an online test -For more details, please write to contact@spoken-tutorial.org |
Slide 18 :
Forum to answer questions
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Slide 19:
Forum to answer questions
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Slide 20:
Lab Migration Project
For more details visit this site: http://cfd.fossee.in/ |
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Slide 21:
Case Study Project
For more details visit this site: http://cfd.fossee.in/ |
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Slide 22:
Acknowledgement
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Spoken Tutorials are part of Talk to a Teacher project,
It is supported by the National Mission on Education through ICT, MHRD, Government of India. More information on the same is available at the following URL http://spoken-tutorial.org/NMEICT-Intro |
About the contributor | This is Rahul Joshi from IIT BOMBAY signing off.
Thanks for joining |