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

Search Results

Register Blogs Community New Posts Updated Threads Search

Showing results 1 to 4 of 4
Search took 0.00 seconds.
Search: Posts Made By: ozturk
Forum: CFX June 6, 2016, 08:55
Replies: 31
Views: 29,604
Posted By ozturk
Hi, Again I am here :) Maybe you can remember...

Hi,
Again I am here :)
Maybe you can remember my model is 3d airfoil. I analize cd nad cl coefficient. I want to ask that I write the area which looking airfoil through y axis. I know this is true...
Forum: CFX April 29, 2016, 05:07
Replies: 31
Views: 29,604
Posted By ozturk
I understood that: I think my way is true....

I understood that: I think my way is true. Because I do not use k-epsilon ( wall function ). I use k-w STT so for my y+ value 1 is right desired value.
Thank you again.
Regards
Forum: CFX April 29, 2016, 03:56
Replies: 31
Views: 29,604
Posted By ozturk
Thanks for your quick reply, You said I should...

Thanks for your quick reply,
You said I should do a mesh sensitivity study; I should run different mesh elements number.
I calculated my case between 2000000 and 4500000 elements and then my max...
Forum: CFX April 28, 2016, 15:23
Replies: 31
Views: 29,604
Posted By ozturk
Is it right value?

Hello,
I am analizing 3d naca airfoil. I use k-w SST and my Re 4.1e+7. I want to learn drag and lift over airfoil. Airflow velocity is 210 m/s. I desired y+ value 1 and calculate my first wall...
Showing results 1 to 4 of 4

 
Forum Jump

All times are GMT -4. The time now is 00:38.