CFD Online Discussion Forums

CFD Online Discussion Forums (https://www.cfd-online.com/Forums/)
-   FLUENT (https://www.cfd-online.com/Forums/fluent/)
-   -   Validation of FLUENT (https://www.cfd-online.com/Forums/fluent/79602-validation-fluent.html)

Destry August 28, 2010 00:45

Validation of FLUENT
 
Dear all...

i just run some cases about fluid flow around cylindrical structure..
how can i know my result valid or not?
how can i know this FLUENT valid?




thank you so much...

Gbu

kingjewel1 August 28, 2010 05:25

Quote:

Originally Posted by Destry (Post 273154)
Dear all...

i just run some cases about fluid flow around cylindrical structure..
how can i know my result valid or not?
how can i know this FLUENT valid?




thank you so much...

Gbu

What type of flow? you may have analytical solution for certain types like laminar or inviscid

Destry August 28, 2010 05:36

Quote:

Originally Posted by kingjewel1 (Post 273159)
What type of flow? you may have analytical solution for certain types like laminar or inviscid


i do analytical solution for inviscid flow...
but from simulation the velocity around the pipe = 0..
but in analytical solution the velocity around pipe = 2*U
U = inflow velocity....

i do the simulation based on FLUENT tutorial....

Destry August 29, 2010 02:18

Quote:

Originally Posted by Destry (Post 273160)
i do analytical solution for inviscid flow...
but from simulation the velocity around the pipe = 0..
but in analytical solution the velocity around pipe = 2*U
U = inflow velocity....

i do the simulation based on FLUENT tutorial....


i also do an analytical solution for 1 case from FLUENT tutorial,,,
when i do comparing,,, the result also give a big difference...
especially on the pipe surface..
but when i do comparing above the pipe,,, it gives close result..
is it the limitation of this program?


thx all

Philipov September 1, 2010 04:21

Give more information.... and beware of the fact that close to obstacles the velocity lim-s to zero....

Destry September 1, 2010 04:46

1 Attachment(s)
Quote:

Originally Posted by Philipov (Post 273574)
Give more information.... and beware of the fact that close to obstacles the velocity lim-s to zero....

inlet velocity= 1 m/s
pipe position in middle of frame...
i also have problem in pressure
also gives a big error (when i comparing to analytical solution)
the analytic solution using superposition of uniform flow+doublet equation...

here i attach velocity contour produce by fluent for my case

Philipov September 1, 2010 05:06

I do not see velocity problems.... check Re and see the flow pattern.... How did you calculate that velocity must be 2*U?!?!? and where it must be so (around where)?

Destry September 1, 2010 05:27

1 Attachment(s)
Quote:

Originally Posted by Philipov (Post 273583)
I do not see velocity problems.... check Re and see the flow pattern.... How did you calculate that velocity must be 2*U?!?!? and where it must be so (around where)?

the velocity must be 2*U*sin (tetha) in pipe's surface
where tetha is the angle to the center of pipe....
i calculate them from the superposition of uniform flow+doublet flow...


here i attach the picture again with the angle

Philipov September 1, 2010 05:41

On the picture you have resultant velocity ( velocity magnitude) and the formula you are looking for "x"... try to show only velocity on x-axis...

Destry September 1, 2010 05:47

1 Attachment(s)
Quote:

Originally Posted by Destry (Post 273587)
the velocity must be 2*U*sin (tetha) in pipe's surface
where tetha is the angle to the center of pipe....
i calculate them from the superposition of uniform flow+doublet flow...


here i attach the picture again with the angle

i calculate the resultan also in analytical not only in x direction....

i also attach the equation here....
thx before

Philipov September 1, 2010 06:12

I am not sure if you can use these equations for all Re range....

Destry September 1, 2010 06:18

Quote:

Originally Posted by Philipov (Post 273595)
I am not sure if you can use these equations for all Re range....



mmmmm


oke,,,
i'll try for smaller Re....
i'll ask u later....


thx for helping


All times are GMT -4. The time now is 19:26.