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-   -   setting the correct format of nonuniform List<vector> for inlet in 0 Folder (http://www.cfd-online.com/Forums/openfoam/121833-setting-correct-format-nonuniform-list-vector-inlet-0-folder.html)

cfdonline2mohsen August 6, 2013 08:12

setting the correct format of nonuniform List<vector> for inlet in 0 Folder
 
Dear All

I have some problem with the correct format of nonuniform List<vector> for my inlet boundary conditions for U in 0 Folder.
I want to specify a nonuniform velocity for U at inlet for my LES calculation from my previous RANS calculations output.
In nonuniform List<vector> we must specify only the U in the inlet faces like this:

Code:

value nonuniform List<vector>
32
(
( 0.125901997 0.138911426 0. )
( 0.128139153 0.172775626 0. )
( 0.126960248 0.211820379 0. )
( 0.120514534 0.254806578 0. )
( 0.107431941 0.30025211 0. )
( 0.0867254138 0.346227229 0. )
( 0.0579536967 0.390691847 0. )
( 0.0212141946 0.431824267 0. )
( 0.138057172 0.00678228773 0. )
( 0.135565937 0.0201092884 0. )
( 0.131116718 0.0328430161 0. )
( 0.126068711 0.0451080948 0. )
( 0.121914245 0.0576611347 0. )
( 0.11977531 0.0717905611 0. )
( 0.120108962 0.0890788361 0. )
( 0.122550257 0.111073039 0. )
( -0.461236358 0.508895934 0. )
( -0.393406957 0.530447841 0. )
( -0.32478264 0.541867137 0. )
( -0.257232815 0.543873072 0. )
( -0.192155391 0.537038386 0. )
( -0.130680457 0.521705806 0. )
( -0.0739541948 0.498558581 0. )
( -0.0230022091 0.468220979 0. )
( -0.802104294 0.0394048579 0. )
( -0.788241446 0.116924562 0. )
( -0.764009297 0.191374391 0. )
( -0.73147279 0.261725157 0. )
( -0.690910041 0.326776087 0. )
( -0.642638564 0.385182768 0. )
( -0.587392509 0.435639977 0. )
( -0.526437223 0.477134943 0. )
);

What I found is that 32 is the number of faces in inlet (not the points) and there is no need to specify the coordinates of the faces but what I don't know is the arrangement of these data in x,y,z directions??what is the coordinates of the related faces and where are these defined so that OF can detect them correctly?
so here is my question:
how can I export my inlet from my previous RANS calculations at the inlet patch to have the above format (i.e. the values of velocities at inlet faces with the OpenFOAM Format) without the need for arranging them manually. since my inlet have more than 4000 faces so it is impossible to do it manually.:confused::confused::confused:
I have used the sampling utility in inlet for my previous calculations but it gave me the values of velocities at points not cells.
Does anybody know how can i do that?
Thanks for your helps in advance.

cfdonline2mohsen August 6, 2013 17:00

I found The Answer.
I write it here for the future use.
The values for all the variables will be written for all the patches (including the inlet patch) in all timesteps (except 0 folders) in the same format that is needed for "nonuniform List<vector>" so I can easily copy them for 0 Folder.
so there is no need for sampling utility.
furthermore I found the answer to my question about sampling by reading the sampleDict headers in src.
in order to sample the data on a surface the following code should be added to controlDict:
Code:

surfaceSampling
    {
        // Sample at inlet

        type surfaces;

        // Where to load it from (if not already in solver)
        functionObjectLibs ("libsampling.so");
        enabled        true;
        outputControl  outputTime;

        interpolationScheme cellPointFace; //cellPoint; //cell; 

        surfaceFormat    foamFile;  //vtk;    foamFile : separate points, faces and values file

        // Fields to be sampled
        fields
        (
            U
            k
            epsilon
        );

        surfaces
        (

    Inlet_constant
    {
        type            patch;
        patches        ( inlet );
        // interpolate    true;    HTRL    If True then the point values will be given not cell values
        // Optional: whether to leave as faces (=default) or triangulate
        // triangulate    false;
    }
        );
    }

}

what I found is that (of course by trial and error method!) if :
Code:

interpolate    true
then the sampling will give the point values at inlet not cell values. so in order to find the cell values the above line should be commented out

Of course as I told before there is a simpler way and therefore no need to use the sampling utility in order to find the corresponding values that must be used with "nonuniform List<vector>"
but the final results for both was the same.

KYPCK444 August 9, 2013 12:30

hi, thanks for sharing your results.

I tried to apply the sample utility to the channel flow case, creating a sampleDict where I define a plane at a certain distance from the outlet:


setFormat raw;

surfaceFormat foamFile;

formatOptions
{
ensight
{
format ascii;
}
}

interpolationScheme cellPoint;

fields
(
p
U
);

surfaces
(
constantPlane
{
type plane;
basePoint (3 0 0);
normalVector (1 0 0);
}
);



I run the solver, then I type:
sample -latestTime
and a directory called surfaces is created, where you can find:
a file called faceCentres which has twice the number of cells (if I have a square grid of 4x4 cells, faceCentres has 32 values);
a file called points where there's the list of the grid points coordinates (25 values if you have a 4x4 grid);
files p and U containing twice the number of cells (32).

What I think I have understood is that by the sample utility (and by the above sampleDict) I obtain values of p and U (and others if you want) at cell centres, not at points.

I am trying to use this "sampled" files to feed another channel flow case at inlet by timeVartingMappedFixedValue, such as in pitzDailyExptInlet tutorial).

The questions are:

how do you manage to get a list of values for p, U, .... fields at a certain section (at inlet, outlet, or middle sections) without sampling utility?

don't you need something like timeVaryingMappedFixedValue or groovyBC boundary patch type to set nonUniform list of values at inlet?

thanks!

cfdonline2mohsen August 9, 2013 17:18

Dear KYPCK444

Quote:

how do you manage to get a list of values for p, U, .... fields at a certain section (at inlet, outlet, or middle sections) without sampling utility?
As I said before, if you open U (or any other field) in your last time step folder you can see that the values for velocity are written for all the patches (including the inlet boundary). just search the inlet keyword (of course by using ctrl+F:)) and the copy and paste the desired value.then go to the 0 folder for your new case, open U and paste them under:
Code:

type fixedValue
value nonuniform List<vector>

for your new inlet patches.

Quote:

don't you need something like timeVaryingMappedFixedValue or groovyBC boundary patch type to set nonUniform list of values at inlet?
If the number of your points are very large; so it is impossible to enter them manually in the correct format that is used by OF.
in this case i use a trick so that i will use timeVaryingMappedFixedValue or groovyBC type for my inlet then i will run my case only for 1 time step then I go to the new time step folder and continue just like that i said above.
The reason for this is that because if I use timeVaryingMappedFixedValue or groovyBC for my inlet since they are a type not value then I can't use other inlet types like directMapped (at least I don't know how to use them simultaniously!!:confused::confused:)

RodriguezFatz September 17, 2013 07:39

Dear Kia,

But what, if the outlet of the source case does not have the same mesh as the inlet of the target case, i.e. meshes are not conformal? I can not just copy the "old" values to the "new" inlet, because number and location of each face differs...

Philipp.

cfdonline2mohsen September 17, 2013 15:55

Dear Philipp
Yeah you are right.I dont know what to do if you want to use the outlet of you case for the inlet of your new case.
Please let me know if you find something.

Sunxing November 26, 2013 03:59

Quote:

Originally Posted by cfdonline2mohsen (Post 444788)
Dear KYPCK444



As I said before, if you open U (or any other field) in your last time step folder you can see that the values for velocity are written for all the patches (including the inlet boundary). just search the inlet keyword (of course by using ctrl+F:)) and the copy and paste the desired value.then go to the 0 folder for your new case, open U and paste them under:
Code:

type fixedValue
value nonuniform List<vector>

for your new inlet patches.


Hi,

I have found that most of the LES tutorials in OF set the inlet velocity as
Code:

    inlet
    {
        type            turbulentInlet;
        referenceField  uniform (10 0 0);
        fluctuationScale (0.02 0.01 0.01);
        value          uniform (10 0 0);
    }

So I want to know did you set your inlet velocity as fixedValue in the new LES case? Have your new LES case given out good result? And can you share us your 0 folder in the new LES case?

Best regards
sunxing


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