CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Swirl-Velocity Specification of 2-D Fan Boundary Condition

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 21, 2018, 03:04
Default Swirl-Velocity Specification of 2-D Fan Boundary Condition
  #1
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
I opened a relevant thread before at the student community forums of ANSYS but did not find a closure about the subject (i.e. https://studentcommunity.ansys.com/t...ary-condition/ ). I'll appreciate any help from the cfd-online community.

I am defined a 2-D fan model using the fan boundary condition on a square surface in a 3-D simulation of a room. I am puzzled by how Fluent interprets the tangential velocity since the tangential velocity I get as a result is always less than what I input, and typically half of the constant value I input as tangential velocity (i.e. when I use values on the order of axial velocity).

The results below correspond to the case with a constant tangential velocity of 1 m/s. According to the plot of tangential velocity as a function of y direction along the midline of the fan surface, the values plateaued at around 0.5 m/s outside hub (half of the input). How should I interpret this?





I'll greatly appreciate your help in clarifying how Fluent uses inputs for tangential velocity in the 2-D fan boundary condition? Why don't I see the tangential velocity imposed between the hub radius and outer dimension of the boundary surface as I define? Is there a physical reasoning behind this?
erdenh is offline   Reply With Quote

Old   September 21, 2018, 11:26
Default
  #2
Senior Member
 
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,674
Rep Power: 65
LuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura about
Which boundary condition are you using? Fluent doesn't have a "fan boundary condition" Just post a screenshot of your boundary condition input.
LuckyTran is offline   Reply With Quote

Old   September 24, 2018, 01:43
Default
  #3
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
Quote:
Originally Posted by LuckyTran View Post
Which boundary condition are you using? Fluent doesn't have a "fan boundary condition" Just post a screenshot of your boundary condition input.
Here is the screenshot of what I use.
Attached Images
File Type: jpg bc.jpg (90.4 KB, 74 views)
erdenh is offline   Reply With Quote

Old   September 28, 2018, 15:25
Default
  #4
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
Any help from the community would be appreciated.
erdenh is offline   Reply With Quote

Old   October 2, 2018, 10:13
Default
  #5
Member
 
yanki cob
Join Date: Jan 2018
Posts: 30
Rep Power: 8
yanki is on a distinguished road
Can you check velocities slightly downstream/upstream of the fan surface?
yanki is offline   Reply With Quote

Old   October 2, 2018, 13:58
Default
  #6
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
Quote:
Originally Posted by yanki View Post
Can you check velocities slightly downstream/upstream of the fan surface?
1. Tangential velocity
2. X velocity
3. Z velocity

at the velocity inlet and fan bc
Attached Images
File Type: jpg swirl_Z_axis_1.0_inlet_fan.jpg (120.1 KB, 37 views)
File Type: jpg swirl_Z_axis_1.0_inlet_fan_xvelocity.jpg (119.7 KB, 26 views)
File Type: jpg swirl_Z_axis_1.0_inlet_fan_zvelocity.jpg (120.2 KB, 23 views)
erdenh is offline   Reply With Quote

Old   October 3, 2018, 08:49
Default
  #7
Member
 
yanki cob
Join Date: Jan 2018
Posts: 30
Rep Power: 8
yanki is on a distinguished road
OK, but can you change the contour plane to another plane that is slightly downstream/upstream of the fan plane? Like, 5mm away from the fan.

Also, why do you have a velocity inlet BC?

Quote:
Originally Posted by erdenh View Post
1. Tangential velocity
2. X velocity
3. Z velocity

at the velocity inlet and fan bc

Last edited by yanki; October 3, 2018 at 08:51. Reason: added
yanki is offline   Reply With Quote

Old   October 3, 2018, 09:23
Default
  #8
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
Quote:
Originally Posted by yanki View Post
OK, but can you change the contour plane to another plane that is slightly downstream/upstream of the fan plane? Like, 5mm away from the fan.

Also, why do you have a velocity inlet BC?
No special reason for using velocity inlet BC. I just used a uniform velocity to be able to see the effect of swirl function in the fan BC.

Attached are contours for 5mm upstream, fan and 5mm downstream with the same scale.

Thanks
Attached Images
File Type: jpg swirl_Z_axis_1.0_5mm_upstream.jpg (123.0 KB, 17 views)
File Type: jpg swirl_Z_axis_1.0_fan.jpg (123.4 KB, 15 views)
File Type: jpg swirl_Z_axis_1.0_5mm_downstream.jpg (150.8 KB, 19 views)
erdenh is offline   Reply With Quote

Old   October 3, 2018, 09:38
Default
  #9
Member
 
yanki cob
Join Date: Jan 2018
Posts: 30
Rep Power: 8
yanki is on a distinguished road
So, the max. velocity 5mm downstream is higher than max. velocity on fan plane, right?

Can you find a plane with the velocity value that you input (1m/s I guess)?

Try to turn OFF the node values.

Quote:
Originally Posted by erdenh View Post
No special reason for using velocity inlet BC. I just used a uniform velocity to be able to see the effect of swirl function in the fan BC.

Attached are contours for 5mm upstream, fan and 5mm downstream with the same scale.

Thanks
yanki is offline   Reply With Quote

Old   October 3, 2018, 10:11
Default
  #10
New Member
 
Join Date: Sep 2018
Posts: 6
Rep Power: 7
erdenh is on a distinguished road
Quote:
Originally Posted by yanki View Post
So, the max. velocity 5mm downstream is higher than max. velocity on fan plane, right?
Correct.

Quote:
Originally Posted by yanki View Post
Can you find a plane with the velocity value that you input (1m/s I guess)?

Try to turn OFF the node values.
I have attached the contour at 25 mm downstream of the fan, where the tangential velocity becomes 1 m/s (node values off). I guess I understand where you are going. Does the fan BC impose the tangential velocity within the first cell downstream of the fan, since the cell size is 25 mm?
Attached Images
File Type: jpg swirl_Z_axis_1.0_25mm_downstream.jpg (188.5 KB, 10 views)
erdenh is offline   Reply With Quote

Old   October 3, 2018, 10:52
Default
  #11
Member
 
yanki cob
Join Date: Jan 2018
Posts: 30
Rep Power: 8
yanki is on a distinguished road
I don't know how the BC works, and couldn't find any explanation on the theory/user guide. But there might be an averaging problem, that's why I asked for turned off nodes.

As I understand, this is not a "problem" for you, you just wanted to make sure that the fan BC works the way it intended to.

Quote:
Originally Posted by erdenh View Post
Correct.



I have attached the contour at 25 mm downstream of the fan, where the tangential velocity becomes 1 m/s (node values off). I guess I understand where you are going. Does the fan BC impose the tangential velocity within the first cell downstream of the fan, since the cell size is 25 mm?
yanki is offline   Reply With Quote

Reply

Tags
3-d simulation, fan boundary condition, swirl, tangential velocity


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
The method on dealing with velocity in static pressure outlet boundary condition mona.li CFX 2 September 30, 2017 01:33
Velocity jump boundary condition ASofia OpenFOAM Programming & Development 0 July 14, 2016 09:01
Problem with assigned inlet velocity profile as a boundary condition Ozgur_ FLUENT 5 August 25, 2015 04:58
CFX fails to calculate a diffuser pipe flow shenying0710 CFX 7 March 26, 2013 04:13
Convective Heat Transfer - Heat Exchanger Mark CFX 6 November 15, 2004 15:55


All times are GMT -4. The time now is 19:00.