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October 7, 2010, 05:25 |
fan boundary condition
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#1 |
New Member
tll
Join Date: Oct 2010
Posts: 11
Rep Power: 16 |
hi ,everyone
does anyone uses the "fan boundary condition" in Fluent software? I need some help in setting the parameter. any help will be appreciated wish all of you This is the first time that I ask a quesion here,my English is not so well,wish you will unstand me well. |
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October 7, 2010, 05:30 |
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#2 |
New Member
tll
Join Date: Oct 2010
Posts: 11
Rep Power: 16 |
any help will be appreciated.Thanks
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December 28, 2010, 07:48 |
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#3 |
New Member
Ravi Kanth B
Join Date: Jul 2010
Posts: 10
Rep Power: 16 |
if you can send me your email id i can send you a notes on how to set up the boundary conditions for the jet fan in fluent
cheers Ravi |
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December 28, 2010, 08:32 |
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#4 | |
New Member
tll
Join Date: Oct 2010
Posts: 11
Rep Power: 16 |
Quote:
Thank you very much for your reply. My email address is blusius@126.com. I am looking forward for your email. Thank you again |
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September 29, 2011, 10:50 |
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#5 | |
New Member
fatimah
Join Date: Sep 2011
Posts: 5
Rep Power: 15 |
Quote:
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September 29, 2011, 17:34 |
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#6 |
Senior Member
Mohammad
Join Date: Feb 2010
Location: Shiraz, Iran
Posts: 108
Rep Power: 16 |
hi,
you can simply define a volume domain and in fluent change it from interior to fan. then set the pressure gradient between two sides of fan and swirl velocity(in 3-d) of rotating fan. then solve and see the results! yours, mohammad |
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September 29, 2011, 23:56 |
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#7 |
New Member
tll
Join Date: Oct 2010
Posts: 11
Rep Power: 16 |
I have no idea about how to set the swirl velocity which contains two component: radial velocity and tangential velocity...can u help me?
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September 30, 2011, 00:00 |
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#8 |
New Member
tll
Join Date: Oct 2010
Posts: 11
Rep Power: 16 |
I only know something about the fan which is supposed to be static in the flow field. if your model is supposed to be swirl in the flow, i do not have much idea about how to set the parameters which are needed by Fluent Solver
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September 30, 2011, 04:32 |
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#9 |
Senior Member
Mohammad
Join Date: Feb 2010
Location: Shiraz, Iran
Posts: 108
Rep Power: 16 |
hi,
I'm not sure but I think you can only set tangential velocity in fan models, not the radial. and the tangential is usually set as the rpm of the fan (propeller,turbine,compressor,...). if I'm not wrong, fluent uses pressure gradient as a pressure jump between two sides of fan zone and adds swirl velocity as V_theta=r*w to the flow. the result should not be so wrong but you know it's just an approximate! yours, mohammad |
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September 30, 2011, 23:39 |
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#10 |
New Member
fatimah
Join Date: Sep 2011
Posts: 5
Rep Power: 15 |
thanks to all.. actually my problem since at Gambit.. Fan is a part of my model.. I try a few method like subtract and split fan from flow field then set up bondary condition.. I dont know ist my problem at modelling or set up boundary condition in gambit.. Please help me..
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May 20, 2012, 08:07 |
Jet Fans BCs Notes
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#11 | |
New Member
Sherif Gomaa
Join Date: May 2012
Posts: 1
Rep Power: 0 |
Quote:
Thank you for your help Sherif |
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June 8, 2013, 05:44 |
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#12 | |
New Member
michelle
Join Date: Jun 2013
Posts: 7
Rep Power: 13 |
Quote:
halo.. may i have the notes that u mention above..? i do appreciate it.. my emel is harmaizura90@gmail.com |
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July 18, 2013, 09:46 |
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#13 |
New Member
Bruce
Join Date: Mar 2012
Posts: 8
Rep Power: 14 |
in the ansys fluent help pdf file , there is a very detailed description of the fan model in the flug.pdf .
good luck ! |
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March 25, 2014, 12:39 |
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#14 |
New Member
Join Date: Feb 2014
Posts: 28
Rep Power: 12 |
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March 26, 2014, 01:11 |
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#15 |
New Member
Ravi Kanth B
Join Date: Jul 2010
Posts: 10
Rep Power: 16 |
please send me your email id. I will see if i can find it for your and send it across.
Regards, Ravi |
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March 26, 2014, 04:09 |
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#16 |
New Member
Join Date: Feb 2014
Posts: 28
Rep Power: 12 |
Hello. Thanks for your reply ! My mail is: guillaume_dlvm@hotmail.fr
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April 15, 2014, 22:06 |
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#17 |
New Member
Join Date: Apr 2013
Posts: 3
Rep Power: 13 |
Greetings;
I´m working on a project in which I have to analyse the flow over a spinning propeller and a cylindric body behind it, I would be really thankful if you could share those FAN notes with me as I was told this Boundary condition could be helpful to my model, thus I´m trying to learn as much as I can about it to model my case. My email is s.gkrlos@hotmail.com |
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April 24, 2014, 06:26 |
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#18 |
New Member
anonymous
Join Date: Apr 2014
Posts: 2
Rep Power: 0 |
hello i need to simulate jet fans can ravi please send me the note too my email is jgd05@mail.aub.edu
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May 12, 2014, 06:48 |
Fan model
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#19 |
New Member
Fyodor Arndt
Join Date: May 2014
Posts: 1
Rep Power: 0 |
Hey Ravi,I am modeling a water tunnel with a fan in it. I have already tried to use the tangential velocity and pressure jump as inputs without being successful. I will be very thankful to you if you send me your fan model to fjodor.arndt@web.de. Thank you in advance.
Cheers |
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August 29, 2014, 13:01 |
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#20 |
New Member
murat akarsu
Join Date: Aug 2014
Posts: 6
Rep Power: 12 |
this is old topic.ı feel lucky.ı want to learn how to analisy and simulationabout centrifugal air fan.is there anoyone to help me by sending notes,video models.thank you so much for interest my gmail adress is murat.akarsu44@gmail.com
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