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CFX Timescale: Difference between Physical,Local facotr and Auto Timescale |
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April 6, 2014, 21:36 |
CFX Timescale: Difference between Physical,Local facotr and Auto Timescale
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#1 |
Member
Faizan
Join Date: Mar 2014
Posts: 76
Rep Power: 12 |
Hi all,
Please suggest me the difference between Physical timescale, Local timescale factor and Auto timescale? first I tried my cfd project with auto timescale, then local timescale factor and then physical timescale. The problem I am having with physical timescale is that it is finishing before the suggested iterations. I set 1000 iterations but with physical timescale the solver stopped after 141 iterations. WHY? I do not understand. Please anyone know the reason then please reply to this post............Humble request..... Thanks in advance |
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April 7, 2014, 02:06 |
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#2 | ||
Senior Member
Join Date: Feb 2011
Posts: 496
Rep Power: 18 |
Quote:
Auto timescale - CFX determines time step automatically based on the boundary conditions, flow conditions, physics, and domain geometry; Local timescale factor - enables different time scales to be used in different regions of the calculation domain. The value you enter is a multiplier of a local element-based time scale. Why don't you use CFX help? Quote:
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April 7, 2014, 02:10 |
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#3 |
Member
Faizan
Join Date: Mar 2014
Posts: 76
Rep Power: 12 |
Thanks Antanas,
What do u suggest that which timescale shud I use for my model. I am modelling a supersonic convergent-divergent nozzle. The gas in nozzle is nitrogen with 1.4MPa total pressure and 550C total temperature inlet boundary condition. I enclosed the nozzle in cylindrical surrounding domain filled with nitrogen gas too with opening boundary condition. Please suggest if physical timescale is OK with my entire flow domain. |
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April 7, 2014, 02:39 |
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#4 | |
Senior Member
Join Date: Feb 2011
Posts: 496
Rep Power: 18 |
Quote:
1. Use auto-timescale. 2. Set appropriate initial distribution. It's more important IMO. You may use gas-dynamic functions for that. 3. Use Upwind scheme to get approximate solution. 4. Use results of step 3 as initial guess and set High Resolution scheme to get final results. You may try to use dt = C * dl / (abs(u)-a), where C <= 1, dl - smallest mesh element dimension, u - characteristic streamwise velocity component, a - characteristic speed of sound. |
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April 7, 2014, 03:03 |
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#5 |
Member
Faizan
Join Date: Mar 2014
Posts: 76
Rep Power: 12 |
Thanks Antanas,
Such a comprehensive response. Sure I would try as u instructed. Cheers, |
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