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why the volume fraction for entire model is not appear

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Old   February 19, 2016, 01:09
Default why the volume fraction for entire model is not appear
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yaseen
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hello
the following images are my model, after 1000 iteration running, the problem is the volume fraction for entire model is not appear (I used volume rendering in CFX post) what is reasons of this???
http://www.cfd-online.com/Forums/att...1&d=1455862066
http://www.cfd-online.com/Forums/att...1&d=1455862080
http://www.cfd-online.com/Forums/att...1&d=1455862099
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File Type: jpg CFX post.jpg (92.9 KB, 43 views)
File Type: jpg CFX pre.jpg (90.3 KB, 36 views)
File Type: png solver.png (47.7 KB, 32 views)
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Old   February 19, 2016, 04:32
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FAQ: http://www.cfd-online.com/Wiki/Ansys...gence_criteria

If those tips do not help then please post your CCL (not screen shots of CFX-Pre, please).
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Old   March 12, 2016, 11:08
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Quote:
Originally Posted by ghorrocks View Post
FAQ: http://www.cfd-online.com/Wiki/Ansys...gence_criteria

If those tips do not help then please post your CCL (not screen shots of CFX-Pre, please).
thanks those tips were usefull, I will try to apply all in my model. finally I will believe my mode should run in transient, the results is good but all equations in solver has no same ratio, only close to each other, what is the reason of this problem? I used 10 sec. as total time, 0.06 sec time step and the Courant Nomber at first iteration is 0.9 but at last iteration RMS Courant No. become 145 and Max. become 999.99 is it Courant No. related to fully convergence?
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Old   March 12, 2016, 16:44
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If it is converging quickly and rapidly despite the high Courant number you should be fine.
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Old   March 13, 2016, 03:02
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no, I said does not converged, I selected time step 0.06 s according to mesh size 0.006 mm (min) and inflow velocity = 0.03m/s, but I dont know velocity in the model entirely, so how can reduced? Courant No, or Courant No. is a reason to the simulation become non converged? thanks
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Old   March 13, 2016, 03:19
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Quote:
I selected time step 0.06 s according to mesh size 0.006 mm (min)
And on what basis does that mean a 0.06s time step is appropriate?

My recommendation for time step size is to use adaptive time steps homing in on 3-5 coeff loops per iteration. Then the solver finds its own time step.
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Old   March 13, 2016, 06:05
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thanks for your recommend, based on Courant No.between (2 - 10)
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Old   March 13, 2016, 06:46
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Unless you have shown that a Courant number of 2-10 is suitable for your simulation then it is meaningless. CFX is an implicit solver and does not have a easily definable stability limit like explicit solvers do. So I recommend you do the adaptive time steps homing in on 3-5 coeff loops per iteration instead.
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Old   March 20, 2016, 13:56
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Quote:
Originally Posted by ghorrocks View Post
Unless you have shown that a Courant number of 2-10 is suitable for your simulation then it is meaningless. CFX is an implicit solver and does not have a easily definable stability limit like explicit solvers do. So I recommend you do the adaptive time steps homing in on 3-5 coeff loops per iteration instead.
I used transient with adaptive time step but courant number at five time step is high (RMS = 40, MAX 999), ass follow
Time steps option - adaptive
first update time - 1s
update frequency - 1
initial time step -0.03 sec
min time step 0.00001 s
max time step 5 s
target min loops 3
target max loops 5
time step decrease factor 0.8
time step increase factor 1.06
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Old   March 20, 2016, 18:45
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If that is converging every time step then it should be fine. Or is it not converging?
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Old   March 21, 2016, 05:16
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Quote:
Originally Posted by ghorrocks View Post
If that is converging every time step then it should be fine. Or is it not converging?
the rates are not same as for all equations only close to each other and RMS are near to the target (1e-5)
note: I choose the initial time step not randomly, but by a number trials and calculation like sensitivity analysis, in my view my mesh is also good
in most time steps equations of velocity (U, V, W) shows (ok not OK), I think this relates to inlet velocity B.C, as in image show i have velocity in (x,z) but for y axis (vertical) is zero. so I enter (U=0.03m/s, V=0, W=0.03m/s) is it x=U, y=V , z=W ? or I should enter value for (U & V) and W=0
thanks
http://www.cfd-online.com/Forums/att...1&d=1458571969

Last edited by yaseen wsu; March 21, 2016 at 09:53.
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Old   March 21, 2016, 17:11
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You have done a sensitivity check on time step - good.

But you should also do one on convergence toleration and mesh size. Your convergence tolerance may be tighter (or looser) than is required, and your mesh may be too coarse or too fine. In this case, as you appear to be using a transient simulation to find the steady state answer you can probably loosen the convergence tolerance - this will help things a lot but you will need to check this before doing it.
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Old   March 21, 2016, 22:22
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thanks, I know how to done senstivity analysis for mesh size, but I dont know sensitivity analysis for convergence toleration, how to done?
thanks
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Old   March 22, 2016, 09:48
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Quote:
Originally Posted by yaseen wsu View Post
thanks, I know how to done senstivity analysis for mesh size, but I dont know sensitivity analysis for convergence toleration, how to done?
thanks
dear yaseen, Please refer to the link below.
http://www.cfd-online.com/Forums/cfx...imbalance.html
hope it helps.
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Old   March 22, 2016, 14:01
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thanks a lot
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