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Divergence and High Aspect Ratios

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Old   April 6, 2013, 17:16
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Quote:
Originally Posted by Far View Post
Because refined mesh is capturing some unsteady flow phenomena which was not being captured in coarse mesh.
I thought the same thing.

I was wondering what value should I be taking for the pressure and velocity? average values?My pressure values are varying from 99200+450.

Also, how do we say it is mesh independent solution? My previous mesh did not have this big oscillation. The pressure was varying from 99010+50.

So, this can be considered mesh independent solution?Also, if my next mesh refinement oscillates more, what mesh I should be taking as final?

Last edited by victoryv; April 7, 2013 at 09:44.
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Old   April 7, 2013, 13:55
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Quote:
Originally Posted by victoryv View Post
I thought the same thing.

My pressure values are varying from 99200+450.

The pressure was varying from 99010+50.
What are the units of pressure? If in "Pa", then you have to look into youe mesh, solution. Something gone wrong.
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Old   April 7, 2013, 14:11
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What are the units of pressure? If in "Pa", then you have to look into youe mesh, solution. Something gone wrong.
Yes the units are in pascal. Why is it wrong?
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Old   April 9, 2013, 15:27
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Can someone suggest me ?
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Old   April 10, 2013, 11:30
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Looks too big number, whats your boundary conditions at inlet. is there any possibility to share your mesh or case files?
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Old   April 10, 2013, 14:01
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Quote:
Originally Posted by Hybrid View Post
Looks too big number, whats your boundary conditions at inlet. is there any possibility to share your mesh or case files?
Boundary conditions are fine. Sen you a mail.

P.S I am monitoring pressure and velocity values at a point
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Old   April 13, 2013, 14:21
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what are the boundary conditions at inlet and outlet
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Old   April 14, 2013, 05:38
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done meshing and solution. Results seem ok and maximum velocity is 70 m/sec


1. Mesh scaled by 0.001 in all directions.

2. Pressure inlet and pressure outlet were used with given boundary conditions

3. Pressure based coupled solver.

4. 2nd order unwind for convection terms

5. pseudo transient and high order term relaxation used

6. Y+ is less than 6 and therefore qualifies for integration to wall approach along with SST turbulence model.

7. Flow is assumed to be incompressible (need confirmation)

Enjoy...









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Old   April 14, 2013, 06:19
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Old   April 14, 2013, 12:54
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Hi Far,

Thank you so much. The results seem to be good.

1. Why did you scale the mesh?
2. I have compressible results to compare with. So I am doing compressible flow.
3.What is this "higher order relaxation" you used?
4.My target is y+<1(or ~1). Also what do you mean by " integration to wall approach" ?
5. Also, by how many lengths did you extend the domain?
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Old   April 14, 2013, 20:00
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Mesh file https://dl.dropboxusercontent.com/u/68746918/WT.msh
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Old   April 14, 2013, 20:09
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I am not able to download the file. Also, can you please email me the file or link instead of uploading here and yeah can you please answer the questions I have asked earlier.
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