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cfd seeker March 2, 2012 09:16

SST kw model
 
Hi all
what will be the consequences if we are using a mesh with y+=5-30 using SST kw in fluent 13 at 4 deg and 12 deg angle of attack? and what will be the consequences if we are using the same mesh at same conditions using Realizable k-e model?
Regards

cfd seeker March 2, 2012 10:42

any body comment please.........

cfd seeker March 3, 2012 11:35

Far where r u lost?? you are lot of experience in this field.......

Far March 3, 2012 14:09

Quote:

what will be the consequences if we are using a mesh with y+=5-30 using SST kw in fluent 13 at 4 deg and 12 deg angle of attack? and what will be the consequences if we are using the same mesh at same conditions using Realizable k-e model?
The results should be similar at 4 and 12 deg for the y+ = 1 and 5-30 if there is no separation. But may start to deviate for y+ 10-30 in comparison to y+ = 1 and 5-10 if separation occurs. According to claim made for the automatic wall treatment it should give you same result for y+ upto 100. But in reality it is not true. If needed I can send you the papers regarding this issue.

cfd seeker March 3, 2012 21:08

Thank you very much Far for your concern, I really appreciate it. Yes papers would have been great help to me, please mail me at yasirforfriends@yahoo.com and by separation you just mean flow separation or you mean stall. Actually in my case, there is flow separation at 12 degree AOA but the wing is not stalling. What exactly you are talking about?

Far March 3, 2012 22:10

Quote:

Originally Posted by cfd seeker (Post 347492)
by separation you just mean flow separation or you mean stall. Actually in my case, there is flow separation at 12 degree AOA but the wing is not stalling. What exactly you are talking about?

I mean separation and for massive separation/stall better model would be the Differential Reynolds stress model, DES and/or LES. As you know, RANS models assume that the turbulence is isotrpic.

cfd seeker March 4, 2012 04:33

So it means even if at 12 degree AOA, wing is not stalling but we have to have wall y+ =1-10 to properly capture the physics of the flow and to get good estimate of CL and CD values right?

Far March 4, 2012 04:44

Quote:

So it means even if at 12 degree AOA, wing is not stalling but we have to have wall y+ =1-10 to properly capture the physics of the flow and to get good estimate of CL and CD values right?
Yes, It is true based on the published results.

But to be sure for your case, you need to run the case with at least two y+ values or probably three i.e. y+ = 1, 10 and 30 for such extreme condition.

Rule of thumb is not meant for the final solution, it just guide you to the destination with minimum hassle, otherwise to be confident, you have to still make some checks for your case.

Also you need to ensure that boundary layer contains at least 10-15 nodes for automatic wall treatment.

I am sending you relevant Journal papers, in order to gain more insight to what I am referring.

cfd seeker March 4, 2012 04:49

thanks alot Far for your concern. Kindly mail me that papers, i have given yahoo id in the above posts

syavash September 21, 2012 10:38

Quote:

Originally Posted by Far (Post 347528)
Yes, It is true based on the published results.

But to be sure for your case, you need to run the case with at least two y+ values or probably three i.e. y+ = 1, 10 and 30 for such extreme condition.

Rule of thumb is not meant for the final solution, it just guide you to the destination with minimum hassle, otherwise to be confident, you have to still make some checks for your case.

Also you need to ensure that boundary layer contains at least 10-15 nodes for automatic wall treatment.

I am sending you relevant Journal papers, in order to gain more insight to what I am referring.

Dear Far,

May you please send me the papers you've discussed above?
My E-mail is syavash_azna@yahoo.com
Tnx in advance.

cartman September 21, 2012 12:08

Dear Far,,,,

I would appreciate your advise

I don't want to bother you, but...

Could you give me the paper please?

That paper seems very useful for my investigation :D

My e-mail adress is hdkam@pknul.ac.kr

Far September 21, 2012 12:13

Quote:

Originally Posted by cartman (Post 382995)
Dear Far,,,,

I would appreciate your advise

I don't want to bother you, but...

Could you give me the paper please?

That paper seems very useful for my investigation :D

My e-mail adress is hdkam@pknul.ac.kr

pls confirm your email address

syavash September 21, 2012 12:29

Quote:

Originally Posted by Far (Post 382996)
pls confirm your email address

My E-mail address is syavash_azna@yahoo.com

tnx again.

Far September 22, 2012 14:27

sent
 
Please check your email.

Far September 22, 2012 14:31

I am getting this error

Quote:

Delivery to the following recipient failed permanently:

hdkam@pknul.ac.kr

Technical details of permanent failure:
DNS Error: Domain name not found


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