Difference between revisions of "OpenFOAM/C2/Simulating-flow-in-a-Lid-Driven-Cavity/English-timed"
From Script | Spoken-Tutorial
PoojaMoolya (Talk | contribs) |
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| In this tutorial I will show you | | In this tutorial I will show you | ||
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| The''' Lid Driven Cavity''' '''file structure''' | | The''' Lid Driven Cavity''' '''file structure''' | ||
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| 00:12 | | 00:12 | ||
| '''Meshing '''the Geometry | | '''Meshing '''the Geometry | ||
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| 00:14 | | 00:14 | ||
| Solving and '''post-processing results''' in '''Paraview''' | | Solving and '''post-processing results''' in '''Paraview''' | ||
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| − | | 00: | + | | 00:17 |
| Plotting '''& '''validating''' results on a '''spreadsheet'''. | | Plotting '''& '''validating''' results on a '''spreadsheet'''. | ||
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| 00:21 | | 00:21 | ||
| To record this tutorial | | To record this tutorial | ||
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| 00:22 | | 00:22 | ||
| I am using '''Linux Operating system Ubuntu version 10.04''' . | | I am using '''Linux Operating system Ubuntu version 10.04''' . | ||
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| '''Lid driven cavity''' is the most widely used '''2D test''' | | '''Lid driven cavity''' is the most widely used '''2D test''' | ||
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| The '''boundary''' '''conditions''' remain the same | | The '''boundary''' '''conditions''' remain the same | ||
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| We are '''solving''' this for '''Reynolds no (Re) = 100''' | | We are '''solving''' this for '''Reynolds no (Re) = 100''' | ||
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| 01:02 | | 01:02 | ||
| − | | To do this press '''Ctrl+Alt+t '''simultaneously on your '''keyboard''' | + | | To do this press '''Ctrl+Alt+t ''' keys simultaneously on your '''keyboard''' |
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| 01:12 | | 01:12 | ||
| − | |Now | + | |Now type '''run''' and press '''enter''' |
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|01:15 | |01:15 | ||
| − | | '''cd '''(space)''' | + | | '''cd '''(space) tutorials''' and Press '''Enter''' |
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| 01:20 | | 01:20 | ||
| − | | '''cd '''(space)''' incompressible and Press | + | | '''cd '''(space)''' incompressible''' and Press '''Enter''' |
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| 01:26 | | 01:26 | ||
| − | |'''cd '''(space)''' icoFoam '''(Note that F here is capital)''' | + | |'''cd '''(space)''' icoFoam '''(Note that F here is capital) and Press '''enter''' |
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| 01:33 | | 01:33 | ||
| − | | ''' cd '''(space) cavity and '''Press Enter''' | + | | ''' cd '''(space) '''cavity and ''' Press '''Enter''' |
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|01:55 | |01:55 | ||
| − | | The '''constant folder '''contains another '''folder''' named '''polymesh | + | | The '''constant folder '''contains another '''folder''' named '''polymesh''' and a file describing the physical properties of fluid. |
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| − | | 02: | + | | 02:01 |
| − | | Now type '''cd (space) polymesh''' and ''' | + | | Now type '''cd (space) polymesh''' and Press '''Enter''' |
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| 02:08 | | 02:08 | ||
| − | | '''Polymesh contains a file named blockMeshDict ''' | + | | '''Polymesh''' contains a file named '''blockMeshDict ''' |
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| 02:12 | | 02:12 | ||
| − | | Now type '''ls''' and press | + | | Now type '''ls''' and press '''Enter''' |
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| 02:17 | | 02:17 | ||
| − | | To open up the '''blockMeshDict'''file type '''gedit blockMeshDict''' | + | | To open up the '''blockMeshDict''' file type '''gedit space blockMeshDict''' |
| + | (Note that M and D here are capital) | ||
| − | ''' | + | Now press '''enter''' |
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| 02:32 | | 02:32 | ||
| − | | | + | | Let me drag this to the capture area |
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| 02:36 | | 02:36 | ||
| − | | This contains : ''' | + | | This contains : cordinates for '''lid driven cavity''' |
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| 02:41 | | 02:41 | ||
| − | |'''blocking and meshing parameters''' | + | |'''blocking''' and '''meshing parameters''' |
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| 02:44 | | 02:44 | ||
| − | |''' | + | |and '''boundary patches.''' |
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| 02:47 | | 02:47 | ||
| − | + | | Since there are no '''arcs''' as well as no '''patches''' to be''' merged''', '''edges''' and '''mergePatchPairs''' can be kept empty | |
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| − | | 02: | + | | 02:56 |
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| Now close this | | Now close this | ||
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| 02:58 | | 02:58 | ||
| − | | | + | | In the '''command terminal''' type : '''cd (space) .. (dot) (dot)''' and press '''enter.''' |
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| 03:04 | | 03:04 | ||
| − | | Do this twice. | + | | Do this twice. You will come back to the''' cavity folder''' |
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| 03:09 | | 03:09 | ||
| − | | Now type '''cd''' (space) '''system''' and press enter, | + | | Now type '''cd''' (space) '''system''' and press '''enter,''' |
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| − | |03: | + | |03:15 |
| − | | Now type '''ls''' press | + | | Now type '''ls''' press '''Enter''' this contains three files |
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| 03:22 | | 03:22 | ||
| − | |'''controlDict, fvSchemes and fvSolutions''' | + | |'''controlDict, fvSchemes''' and '''fvSolutions''' |
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| 03:30 | | 03:30 | ||
|'''fvSolution''' contains '''discritization schemes''' used in '''run time'''. | |'''fvSolution''' contains '''discritization schemes''' used in '''run time'''. | ||
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| 03:35 | | 03:35 | ||
| − | |And'''fvSchemes''' contains equation for '''solver''', | + | |And '''fvSchemes''' contains equation for '''solver''', '''tolerance''' etc. |
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| 03:40 | | 03:40 | ||
| − | | Now again type '''cd (space) (dot dot) . . '''and press | + | | Now again type '''cd (space) (dot dot) . . '''and press '''Enter''' |
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| − | | 03: | + | | 03:46 |
| − | | Now type '''cd ( space )''' 0 (zero) and Press | + | | Now type '''cd ( space )''' 0 (zero) and Press '''Enter''' |
|- | |- | ||
|03:53 | |03:53 | ||
| − | | Now type''' ls''' and press | + | | Now type''' ls''' and press '''Enter''' |
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| 03:57 | | 03:57 | ||
| − | | This contains the '''initial values''' for '''boundary conditions''' like | + | | This contains the '''initial values''' for '''boundary conditions''' like '''Pressure ,Velocity,Temperature etc.''' |
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| 04:09 | | 04:09 | ||
| Now we need to '''mesh '''the''' geometry''' | | Now we need to '''mesh '''the''' geometry''' | ||
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| 04:11 | | 04:11 | ||
| − | | | + | |We are using a course mesh here. |
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|04:18 | |04:18 | ||
| − | | Now type '''blockMesh '''(Note that M here is capital) and press | + | | Now type '''blockMesh '''(Note that M here is capital) and press '''Enter''' |
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| 04:25 | | 04:25 | ||
| − | | The'''Meshing''' is done. | + | | The '''Meshing''' is done. |
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| 04:31 | | 04:31 | ||
| To view the '''geometry''' | | To view the '''geometry''' | ||
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| 04:32 | | 04:32 | ||
| − | |Type '''paraFoam''' , Note that '''F''' here is '''capital''' and ''' | + | |Type '''paraFoam''' , Note that '''F''' here is '''capital''' and press '''Enter''' |
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|04:58 | |04:58 | ||
| Check the mesh by typing '''checkMesh''' in the''' terminal''' | | Check the mesh by typing '''checkMesh''' in the''' terminal''' | ||
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| 05:04 | | 05:04 | ||
| − | |Note that '''M''' here is capital and press | + | |Note that '''M''' here is capital and press '''Enter''' |
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|05:08 | |05:08 | ||
| − | | you can see the | + | | you can see the number of cells, '''skewness''' and other parameters, which are associated with the '''mesh''' |
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| − | | 05: | + | | 05:17 |
| The solver we are using here is '''icoFoam''' : | | The solver we are using here is '''icoFoam''' : | ||
|- | |- | ||
| 05:20 | | 05:20 | ||
| − | | | + | | '''icoFoam is a Transient''' '''solver''' for '''incompressible flow''' of '''newtonian fluids''' |
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| 05:29 | | 05:29 | ||
| In the '''terminal '''type '''icoFoam''' | | In the '''terminal '''type '''icoFoam''' | ||
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| 05:33 | | 05:33 | ||
| − | |Note that '''F''' here is '''capital''' and press | + | |Note that '''F''' here is '''capital''' and press '''Enter''' |
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| 05:40 | | 05:40 | ||
| − | | After the solving is done type '''paraFoam''' in the terminal | + | | After the solving is done type '''paraFoam''' in the terminal to view the '''geometry''' and the '''results''' |
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| 05:54 | | 05:54 | ||
| On the left hand side of '''object inspector menu''' | | On the left hand side of '''object inspector menu''' | ||
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| 05:57 | | 05:57 | ||
| − | |''' | + | |click on '''Apply''' |
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| − | | 05: | + | | 05:58 |
| Now '''Scroll''' down the '''properties ''' on '''objector inspector menu ''' | | Now '''Scroll''' down the '''properties ''' on '''objector inspector menu ''' | ||
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| 06:02 | | 06:02 | ||
| − | | | + | |you can see '''mesh parts,volume fields etc''' |
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| 06:07 | | 06:07 | ||
| − | | '''Check or uncheck '''these '''boxes''' in the '''mesh''' part | + | | '''Check or uncheck '''these '''boxes''' in the '''mesh''' part, to view the '''different boundary''' '''regions '''of '''Lid driven cavity''' |
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| 06:15 | | 06:15 | ||
| − | | Now after this on top of the left-hand side''' | + | | Now after this on top of the left-hand side on '''active variable control ''', dropdown menu change this from solid color to p or capital U, which are the '''initial conditions''' such as '''pressure , velocity''' |
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| 06:31 | | 06:31 | ||
| − | | | + | |I will select capital U. Now this will show you the initial condition of velocity |
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| 06:37 | | 06:37 | ||
| − | | | + | | On top of the''' paraview window''' you can see the''' VCR control''' |
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| 06:44 | | 06:44 | ||
| − | | | + | |Click on the play button |
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| 07:09 | | 07:09 | ||
| − | |To do this let us '''plot''' the '''U and V velocity''' | + | |To do this let us '''plot''' the '''U''' and '''V velocity''' |
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| 07:25 | | 07:25 | ||
| Select the '''X & Y axis''' turn by turn. | | Select the '''X & Y axis''' turn by turn. | ||
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| 07:37 | | 07:37 | ||
| − | | You can see '''Pressure and velocity''' '''plots''' being plotted | + | | You can see '''Pressure''' and '''velocity''' '''plots''' being plotted |
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| 07:42 | | 07:42 | ||
| − | | Since it is a '''non dimensional analysis''' | + | | Since it is a '''non dimensional analysis''', we need to '''plot the graph''' for '''u/U v/s y/L''' for '''Reynolds number =100''' |
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| 07:52 | | 07:52 | ||
| − | | | + | | To do this in '''Plot Data''' click on the '''Y-axis''' |
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| 08:01 | | 08:01 | ||
| You can see the''' plot''' | | You can see the''' plot''' | ||
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| 08:09 | | 08:09 | ||
| − | | Give | + | | Give appropriate name to your file |
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| 08:11 | | 08:11 | ||
| I will give this as '''cavity''' | | I will give this as '''cavity''' | ||
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| 08:23 | | 08:23 | ||
| Now go to the '''cavity folder''' of '''openfoam directory'''. | | Now go to the '''cavity folder''' of '''openfoam directory'''. | ||
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| 08:39 | | 08:39 | ||
| In the libreoffice spreadsheet copy the U0 (u velocity) and to the right point 1(Y-axis) columns | | In the libreoffice spreadsheet copy the U0 (u velocity) and to the right point 1(Y-axis) columns | ||
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| 08:48 | | 08:48 | ||
| − | | Now divide both these coloumns | + | | Now divide both these coloumns that is '''u zero''' by '''capital U''' and '''points 1''' by '''capital L''' |
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| 09:08 | | 09:08 | ||
| − | + | | Now let me switch back to the slides | |
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| − | | 09: | + | | 09:10 |
| Results obtained will be similar to this figure | | Results obtained will be similar to this figure | ||
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| 09:16 | | 09:16 | ||
| '''Validate''' the result on a paper published on '''Lid Driven Cavity by : Ghia et al. (1982''') and | | '''Validate''' the result on a paper published on '''Lid Driven Cavity by : Ghia et al. (1982''') and | ||
| − | + | Results '''obtained from Fluent''' | |
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| 09:26 | | 09:26 | ||
| − | | | + | |File structure of '''Lid Driven cavity''' |
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| 09:32 | | 09:32 | ||
| − | |And'''Validation''' | + | |And '''Validation''' |
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| 09:41 | | 09:41 | ||
| − | |* '''Kinematic viscosity in transportPorpoerties | + | |* '''Kinematic viscosity''' in '''transportPorpoerties''' in constant folder |
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| 09:45 | | 09:45 | ||
|And Plot results of '''u/U and y/L''' | |And Plot results of '''u/U and y/L''' | ||
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Revision as of 17:49, 23 October 2015
| Time | Narration |
| 00:01 | Hello and welcome to the spoken tutorial on Simulating Flow in a Lid Driven Cavity using openfoam |
| 00:07 | In this tutorial I will show you |
| 00:09 | The Lid Driven Cavity file structure |
| 00:12 | Meshing the Geometry |
| 00:14 | Solving and post-processing results in Paraview |
| 00:17 | Plotting & validating results on a spreadsheet. |
| 00:21 | To record this tutorial |
| 00:22 | I am using Linux Operating system Ubuntu version 10.04 . |
| 00:27 | OpenFOAM version 2.1.0 ParaView version 3.12.0 |
| 00:32 | Lid driven cavity is the most widely used 2D test |
| 00:36 | case for validation of a CFD code |
| 00:39 | This is diagram of Lid Driven Cavity |
| 00:41 | The boundary conditions remain the same |
| 00:44 | A moving wall and three fixedwalls |
| 00:46 | We are solving this for Reynolds no (Re) = 100 |
| 00:50 | The moving wall has a velocity of 1 meters per second |
| 00:54 | The path for the Lid Driven Cavity is the same as discussed in the installation tutorial |
| 01:00 | Now Open a command terminal |
| 01:02 | To do this press Ctrl+Alt+t keys simultaneously on your keyboard |
| 01:08 | In the command terminal type the path for lid driven cavity |
| 01:12 | Now type run and press enter |
| 01:15 | cd (space) tutorials and Press Enter |
| 01:20 | cd (space) incompressible and Press Enter |
| 01:26 | cd (space) icoFoam (Note that F here is capital) and Press enter |
| 01:33 | cd (space) cavity and Press Enter |
| 01:38 | Now type ls and press enter |
| 01:41 | In the file structure of cavity you will see 3 folders : 0 , constant , and system |
| 01:46 | Now type cd (space) constant and press enter |
| 01:52 | Now type ls and press enter |
| 01:55 | The constant folder contains another folder named polymesh and a file describing the physical properties of fluid. |
| 02:01 | Now type cd (space) polymesh and Press Enter |
| 02:08 | Polymesh contains a file named blockMeshDict |
| 02:12 | Now type ls and press Enter |
| 02:15 | You can see the blockMeshDict |
| 02:17 | To open up the blockMeshDict file type gedit space blockMeshDict
(Note that M and D here are capital) Now press enter |
| 02:30 | This will Open up the blockMeshDict file
|
| 02:32 | Let me drag this to the capture area |
| 02:36 | This contains : cordinates for lid driven cavity |
| 02:41 | blocking and meshing parameters |
| 02:44 | and boundary patches. |
| 02:47 | Since there are no arcs as well as no patches to be merged, edges and mergePatchPairs can be kept empty |
| 02:56 | Now close this |
| 02:58 | In the command terminal type : cd (space) .. (dot) (dot) and press enter. |
| 03:04 | Do this twice. You will come back to the cavity folder |
| 03:09 | Now type cd (space) system and press enter, |
| 03:15 | Now type ls press Enter this contains three files |
| 03:22 | controlDict, fvSchemes and fvSolutions |
| 03:26 | controlDict contains control parameters for start/end time.
|
| 03:30 | fvSolution contains discritization schemes used in run time. |
| 03:35 | And fvSchemes contains equation for solver, tolerance etc. |
| 03:40 | Now again type cd (space) (dot dot) . . and press Enter |
| 03:46 | Now type cd ( space ) 0 (zero) and Press Enter |
| 03:53 | Now type ls and press Enter |
| 03:57 | This contains the initial values for boundary conditions like Pressure ,Velocity,Temperature etc. |
| 04:03 | Now Type cd ( space ) (dot dot) . . to return back to the cavity folder |
| 04:09 | Now we need to mesh the geometry |
| 04:11 | We are using a course mesh here. |
| 04:14 | Mesh the geometry by typing blockMesh in the terminal. |
| 04:18 | Now type blockMesh (Note that M here is capital) and press Enter |
| 04:25 | The Meshing is done. |
| 04:27 | If there is some error in the blockMesh file it will be shown in the terminal |
| 04:31 | To view the geometry |
| 04:32 | Type paraFoam , Note that F here is capital and press Enter |
| 04:40 | This will open the paraview window |
| 04:44 | Now on the left hand side of the object inspector menu click on Apply. |
| 04:49 | You can see the lid driven cavity geometry now close this |
| 04:58 | Check the mesh by typing checkMesh in the terminal |
| 05:04 | Note that M here is capital and press Enter |
| 05:08 | you can see the number of cells, skewness and other parameters, which are associated with the mesh |
| 05:15 | Let me switch back to the slides. |
| 05:17 | The solver we are using here is icoFoam : |
| 05:20 | icoFoam is a Transient solver for incompressible flow of newtonian fluids |
| 05:26 | Let me switch back to the terminal |
| 05:29 | In the terminal type icoFoam |
| 05:33 | Note that F here is capital and press Enter |
| 05:37 | The Iterations running will be seen in the terminal window. |
| 05:40 | After the solving is done type paraFoam in the terminal to view the geometry and the results |
| 05:54 | On the left hand side of object inspector menu |
| 05:57 | click on Apply |
| 05:58 | Now Scroll down the properties on objector inspector menu
|
| 06:02 | you can see mesh parts,volume fields etc |
| 06:07 | Check or uncheck these boxes in the mesh part, to view the different boundary regions of Lid driven cavity |
| 06:15 | Now after this on top of the left-hand side on active variable control , dropdown menu change this from solid color to p or capital U, which are the initial conditions such as pressure , velocity |
| 06:31 | I will select capital U. Now this will show you the initial condition of velocity |
| 06:37 | On top of the paraview window you can see the VCR control |
| 06:44 | Click on the play button |
| 06:47 | Now this is the final result of velocity for lid driven cavity |
| 06:52 | Toggle on the color legend by clicking on the top left of the active variable control menu |
| 07:03 | This is the color legend for U velocity |
| 07:07 | We need to validate the results obtained
|
| 07:09 | To do this let us plot the U and V velocity
|
| 07:12 | To do this Go to Filters scroll down > Data Analysis > Plot Over line |
| 07:21 | Click on it |
| 07:23 | You can see X , Y and Z axis |
| 07:25 | Select the X & Y axis turn by turn. |
| 07:31 | I will select the X axis and click Apply |
| 07:37 | You can see Pressure and velocity plots being plotted |
| 07:42 | Since it is a non dimensional analysis, we need to plot the graph for u/U v/s y/L for Reynolds number =100 |
| 07:52 | To do this in Plot Data click on the Y-axis |
| 07:58 | And click APPLY |
| 08:01 | You can see the plot |
| 08:03 | Now in menu bar go to File > Save Data |
| 08:09 | Give appropriate name to your file |
| 08:11 | I will give this as cavity |
| 08:15 | The file will be saved as .csv file |
| 08:19 | Now click ok. Again click ok |
| 08:23 | Now go to the cavity folder of openfoam directory. |
| 08:29 | Scroll down you can see the cavity.csv file |
| 08:34 | Open it in Open office or LibreOffice Spreadsheet |
| 08:39 | In the libreoffice spreadsheet copy the U0 (u velocity) and to the right point 1(Y-axis) columns
in another spreadsheet |
| 08:48 | Now divide both these coloumns that is u zero by capital U and points 1 by capital L |
| 08:59 | And Plot the results in libreoffice charts option on top in the menu bar. |
| 09:08 | Now let me switch back to the slides |
| 09:10 | Results obtained will be similar to this figure |
| 09:16 | Validate the result on a paper published on Lid Driven Cavity by : Ghia et al. (1982) and
Results obtained from Fluent |
| 09:24 | In this tutorial we learnt |
| 09:26 | File structure of Lid Driven cavity |
| 09:28 | Solved lid driven cavity. |
| 09:30 | Post-processing of solutions |
| 09:32 | And Validation |
| 09:34 | As as Assignment, |
| 09:35 | Change some parameters in the lid driven cavity |
| 09:38 | * Velocity Magnitude in the 0 folder |
| 09:41 | * Kinematic viscosity in transportPorpoerties in constant folder |
| 09:45 | And Plot results of u/U and y/L |
| 09:50 | Watch the video available at this URL: http://spoken-tutorial.org/What_is_a_Spoken_Tutorial |
| 09:54 | It summarizes the Spoken Tutorial project. |
| 09:57 | If you do not have good bandwidth, you can download and watch it. |
| 10:00 | The Spoken Tutorial Project Team |
| 10:02 | Conducts workshops using spoken tutorials |
| 10:05 | Gives certificates to those who pass an online test |
| 10:09 | For more details, please write to us at contact @spoken-tutorial.org |
| 10:15 | Spoken Tutorials are part of Talk to a Teacher project, |
| 10:18 | It is supported by the National Mission on Education through ICT, MHRD, Government of India. |
| 10:23 | More information on the same is available at the following URL link http://spoken-tutorial.org/NMEICT-Intro |
| 10:27 | This is Rahul Joshi from IIT BOMBAY signing off. |
| 10:30 | Thanks for joining |
Contributors and Content Editors
DeepaVedartham, Gaurav, Nancyvarkey, PoojaMoolya, Sandhya.np14, Sneha