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Search: Posts Made By: nvtrieu
Forum: FLUENT May 17, 2013, 10:59
Replies: 20
Views: 5,536
Posted By nvtrieu
Hi blackmask, I am only CFD learner guy :) ...

Hi blackmask,

I am only CFD learner guy :)
And I am interested in CFD.
Thanks for your comment on Textbook about CFD of David Wilcox. I just found the copy of this book. It should be useful for...
Forum: FLUENT May 17, 2013, 03:39
Replies: 20
Views: 5,536
Posted By nvtrieu
I would highly recommend you to send me an email...

I would highly recommend you to send me an email about the detail report of you simulation!
here is my email add: trieuckgt@gmail.com
thanks you in advance!
Forum: FLUENT May 17, 2013, 03:34
Replies: 20
Views: 5,536
Posted By nvtrieu
your simulation is 2D or 3D? How is the...

your simulation is 2D or 3D?
How is the geometry/mesh look like?
How much y plus value for the mesh?
Which turbulent model you used? and the setting parameters for the turbulent model?
the...
Forum: FLUENT May 17, 2013, 03:29
Replies: 20
Views: 5,536
Posted By nvtrieu
Hi farzadpourfattah, The wing has been...

Hi farzadpourfattah,

The wing has been already subtracted from the fluid domain. However, I you see from the picture, it it the side surface of wing tip. As I mentioned, the wing is located in the...
Forum: FLUENT May 14, 2013, 23:02
Replies: 20
Views: 5,536
Posted By nvtrieu
you can take a look at these photos

you can take a look at these photos
Forum: FLUENT May 14, 2013, 23:00
Replies: 20
Views: 5,536
Posted By nvtrieu
more information (continue)

more information (continue)
Forum: FLUENT May 14, 2013, 22:57
Replies: 20
Views: 5,536
Posted By nvtrieu
more information

more information
Forum: FLUENT May 14, 2013, 22:36
Replies: 20
Views: 5,536
Posted By nvtrieu
sorry I forgot attach the images!

sorry I forgot attach the images!
Forum: FLUENT May 14, 2013, 22:33
Replies: 20
Views: 5,536
Posted By nvtrieu
hi farzadpourfattah, I checked the y+ value...

hi farzadpourfattah,

I checked the y+ value on the wing surface and it is always smaller than 2 as you can see from the attach image.
The Reynolds number is calculated using chord length: ...
Forum: FLUENT May 14, 2013, 09:35
Replies: 20
Views: 5,536
Posted By nvtrieu
Hi Davidwilcox, Thanks for your very quick...

Hi Davidwilcox,

Thanks for your very quick comment!
I am running simulation using k-w SST now. At AoA=30deg, the solution seems not convergence. After 5000 iterations, the residuals are still...
Forum: FLUENT May 13, 2013, 23:38
Replies: 20
Views: 5,536
Posted By nvtrieu
Simulate NACA 0012 Wing

Hi every one,

I am doing simulation the turbulent flow over NACA 0012 wing at Re 1.2e5.

I want to check the Cd/Cl at various AoA and then compare with experimental data from NACA foils (theory...
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