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January 18, 2021, 14:29 |
Cylinder in Openfoam blockMesh
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#1 |
New Member
Join Date: Nov 2020
Posts: 14
Rep Power: 6 |
Hi All,
I am trying to create an cylinder using blockMesh, I got 3/4 the way through and noticed that it does not line up properly (shown in the image below). Does anyone know why this is the case? Code:
convertToMeters 0.01; //..................................// // Dimensions of the cylinder: cx 5; cy 5; cz 1.0; cylinderThickness 1.0; r 0.5; //..................................// // Calculations for cylinder geometry: h #calc "$cylinderThickness+$cz"; tph #calc "$cylinderThickness+$cz+$cz"; vx #calc "$cx+$r"; nvx #calc "$cx-$r"; vy #calc "$cy+$r"; nvy #calc "$cy-$r"; // Calculations for arcs: c1 #calc "$cx + ($r*cos(45.0))"; //cosine in first quadrant s1 #calc "$cy + ($r*sin(45.0))"; //sine in first quadrant c2 #calc "$cx + ($r*cos(135.0))"; //cosine in first quadrant s2 #calc "$cy + ($r*sin(135.0))"; //sine in first quadrant c3 #calc "$cx + ($r*cos(225.0))"; //cosine in first quadrant s3 #calc "$cy + ($r*sin(225.0))"; //sine in first quadrant c4 #calc "$cx + ($r*cos(315.0))"; //cosine in first quadrant s4 #calc "$cy + ($r*sin(315.0))"; //sine in first quadrant vertices ( // Vertices for the cylinder : // x y z ($vx $cy $cz) ($cx $vy $cz) ($nvx $cy $cz) ($cx $nvy $cz) ($vx $cy $h) ($cx $vy $h) ($nvx $cy $h) ($cx $nvy $h) ($cx $cy $cz) ($cx $cy $h) ); // These are all the 'blocks' in our geometry. blocks ( hex ( 0 1 8 8 4 5 9 9 ) pores ( 25 25 25 ) simpleGrading (1 1 1) hex ( 1 2 8 8 5 6 9 9 ) pores ( 25 25 25 ) simpleGrading (1 1 1) hex ( 2 3 8 8 6 7 9 9 ) pores ( 25 25 25 ) simpleGrading (1 1 1) ); // Edges is a dictionary where we define arcs between vertices. edges ( arc 0 1 ($c1 $s1 $cz) arc 1 2 ($c2 $s2 $cz) arc 2 3 ($c3 $s3 $cz) arc 4 5 ($c1 $s1 $h) arc 5 6 ($c2 $s2 $h) arc 6 7 ($c3 $s3 $h) ); // Boundaries is where we define our boundary patches. boundary ( wall { type wall; faces ( (0 8 8 1) (1 8 8 2) (2 8 8 3) ); } atmosphere { type patch; faces ( (5 9 9 4) (6 9 9 5) (7 9 9 6) ); } sides { type patch; faces ( (0 1 5 4) (2 6 5 1) (3 7 6 2) ); } ); mergePatchPairs ( ); |
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January 19, 2021, 04:57 |
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#2 |
Member
Lilian Chabannes
Join Date: Apr 2017
Posts: 58
Rep Power: 9 |
Your mesh does not load in Paraview for me.
What I can propose is just to make 1/4 of the cylinder and then mirror the mesh twice, it will avoid you the troubles of making 4 blocks. Here is a blockMesh I found in this forum some time ago: Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.0 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object blockMeshDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // //======================== // CONTROLS // number of cells Nx 50; NRinner 15; NRouter 15; // size ratio of cell at the wall to the free-stream one in the near-wall blocks expRatWall 0.1; // for BL expRatWall2 0.1; // pipe-axis direction //======================== convertToMeters 0.001; // all the vertices are in non-dimensional units // pipe assumed to have length and radius of 1 vertices ( (0.00000e+00 0.00000e+00 0.00000e+00) (0.00000e+00 0.00000e+00 8.00000e-01) (0.00000e+00 0.00000e+00 1.00000e+00) (0.00000e+00 6.10535e-01 6.10532e-01) (0.00000e+00 8.00000e-01 0.00000e+00) (0.00000e+00 1.00000e+00 0.00000e+00) (0.00000e+00 7.07107e-01 7.07107e-01) (1 0.00000e+00 0.00000e+00) (1 0.00000e+00 8.00000e-01) (1 0.00000e+00 1.00000e+00) (1 6.10535e-01 6.10532e-01) (1 8.00000e-01 0.00000e+00) (1 1.00000e+00 0.00000e+00) (1 7.07107e-01 7.07107e-01) ); blocks ( hex (0 7 11 4 1 8 10 3) ($Nx $NRinner $NRinner) simpleGrading ($expRatWall2 1 1) hex (4 11 12 5 3 10 13 6) ($Nx $NRouter $NRinner) simpleGrading ($expRatWall2 $expRatWall 1) hex (3 10 13 6 1 8 9 2) ($Nx $NRouter $NRinner) simpleGrading ($expRatWall2 $expRatWall 1) ); edges ( BSpline 1 3 ( //(0.00000e+00 0.00000e+00 8.00000e-01) (0.00000e+00 1.12269e-01 7.92025e-01) (0.00000e+00 2.22463e-01 7.62587e-01) (0.00000e+00 3.26692e-01 7.24996e-01) (0.00000e+00 4.21177e-01 6.86516e-01) (0.00000e+00 5.02076e-01 6.52300e-01) (0.00000e+00 5.66526e-01 6.25913e-01) (0.00000e+00 6.10535e-01 6.10532e-01) ) BSpline 3 4 ( (0.00000e+00 6.10532e-01 6.10535e-01) (0.00000e+00 6.25913e-01 5.66526e-01) (0.00000e+00 6.52300e-01 5.02076e-01) (0.00000e+00 6.86516e-01 4.21177e-01) (0.00000e+00 7.24996e-01 3.26692e-01) (0.00000e+00 7.62587e-01 2.22463e-01) (0.00000e+00 7.92025e-01 1.12269e-01) //(0.00000e+00 8.00000e-01 0.00000e+00) ) BSpline 8 10 ( //(1 0.00000e+00 8.00000e-01) (1 1.12269e-01 7.92025e-01) (1 2.22463e-01 7.62587e-01) (1 3.26692e-01 7.24996e-01) (1 4.21177e-01 6.86516e-01) (1 5.02076e-01 6.52300e-01) (1 5.66526e-01 6.25913e-01) (1 6.10535e-01 6.10532e-01) ) BSpline 10 11 ( (1 6.10532e-01 6.10535e-01) (1 6.25913e-01 5.66526e-01) (1 6.52300e-01 5.02076e-01) (1 6.86516e-01 4.21177e-01) (1 7.24996e-01 3.26692e-01) (1 7.62587e-01 2.22463e-01) (1 7.92025e-01 1.12269e-01) //(1 8.00000e-01 0.00000e+00) ) arc 2 6 (0 0.38268343236508978 0.92387953251128674) arc 6 5 (0 0.92387953251128674 0.38268343236508978) arc 9 13 (1 0.38268343236508978 0.92387953251128674) arc 13 12 (1 0.92387953251128674 0.38268343236508978) ); boundary ( inlet { type patch; faces ( (1 2 6 3) (3 6 5 4) (0 1 3 4) ); } outlet { type patch; faces ( (11 10 8 7) (12 13 10 11) (13 9 8 10) ); } wall { type wall; faces ( (9 13 6 2) (13 12 5 6) ); } symmetryVer { type symmetryPlane; faces ( (2 9 8 1) (1 8 7 0) ); } symmetryHor { type symmetryPlane; faces ( (11 4 0 7) (12 5 4 11) ); } ); mergePatchPairs ( ); // ************************************************************************* // Code:
blockMesh transformPoints -scale "(55 5.5 5.5)" sed -i "s/normalVector.*;/normalVector (0 0 1);/g" system/mirrorMeshDict mirrorMesh -overwrite sed -i "s/normalVector.*;/normalVector (0 1 0);/g" system/mirrorMeshDict mirrorMesh -overwrite # if direction of flow is : z+ transformPoints -rollPitchYaw "(0 -90 0)" # z+ #transformPoints -rollPitchYaw "(0 90 0)" # z- transformPoints -translate "(0 0 -0.0553)" # renumber to optimise parallel running renumberMesh -overwrite
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October 10, 2022, 22:35 |
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#3 | |
Member
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You should add the arc for the fourth quarter as highlighted in red below
Quote:
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October 27, 2022, 17:39 |
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#4 |
New Member
IIIIKEK
Join Date: Oct 2022
Posts: 6
Rep Power: 4 |
I've tried to make cylinder channel, my experience tells me that this must be most smooth way but there is a singularity on centre. Is there easy way to fix it?
Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Website: https://openfoam.org | | \\ / A nd | Version: 9 | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { format ascii; class dictionary; object blockMeshDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // convertToMeters 0.0002; vertices ( (0 -1 0) (40 -1 0) (40 0 -1) (0 0 -1) (0 0 0) (40 0 0) (40 0 0) (0 0 0) (0 0 1) (40 0 1) (0 0 0) (40 0 0) (40 1 0) (0 1 0) ); blocks ( hex (0 1 2 3 4 5 6 7) (1 20 20) simpleGrading (1 1 1) hex (0 1 5 4 8 9 6 7) (1 20 20) simpleGrading (1 1 1) hex (7 6 11 10 8 9 12 13) (1 20 20) simpleGrading (1 1 1) hex (3 2 12 13 7 6 11 10) (1 20 20) simpleGrading (1 1 1) ); edges ( arc 0 3 (0 -0.707107 -0.707107) arc 1 2 (40 -0.707107 -0.707107) arc 0 8 (0 -0.707107 0.707107) arc 1 9 (40 -0.707107 0.707107) arc 8 13 (0 0.707107 0.707107) arc 9 12 (40 0.707107 0.707107) arc 3 13 (0 0.707107 -0.707107) arc 2 12 (40 0.707107 -0.707107) ); boundary ( inlet { type patch; faces ( (0 3 7 4) (3 13 10 7) (7 10 13 8) (0 4 7 8) ); } outlet { type patch; faces ( (1 2 6 5) (2 12 11 6) (6 11 12 9) (1 5 6 9) ); } walls { type wall; faces ( (0 1 9 8) (3 2 12 13) ); } frontAndBack { type wall; faces ( (3 2 1 0) (13 12 9 8) ); } ); mergePatchPairs ( ); // ************************************************************************* // |
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October 28, 2022, 06:28 |
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#5 |
Senior Member
Yann
Join Date: Apr 2012
Location: France
Posts: 1,207
Rep Power: 28 |
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October 29, 2022, 12:11 |
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#6 | |
New Member
IIIIKEK
Join Date: Oct 2022
Posts: 6
Rep Power: 4 |
Quote:
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Tags |
blockmesh, blockmesh cylinder, openfoam |
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