|
[Sponsors] |
May 4, 2017, 12:26 |
Spalart allmaras
|
#1 |
New Member
Jesús Miguel
Join Date: Dec 2016
Posts: 8
Rep Power: 9 |
Hello everyone,
I am trying to run a simulation on starting and stopping vortices of a given airfoil. I chose the Spalart-Allmaras method in the simpleFoam algorithm. These are my question. 1. Meaning of nut and nuTilda. 2. Do I have to type unsteadyState in order to take the temporal term of the equation into account? (I have the answer, thanks in advance to everyone) 3. How do I make the velocity to accelerate suddenly and then stops just for me to prove that those vortices exist and, therefore, the net circulation value is 0. thank you for your help guys. Last edited by jesumi; May 4, 2017 at 12:39. Reason: Found one doubt |
|
May 11, 2017, 18:08 |
|
#2 |
Member
Ran
Join Date: Aug 2016
Posts: 69
Rep Power: 10 |
Greeting jesumi:
1. nut is the eddy viscosity. It describes the transfer of the momentum in the flow. nuTilda is the modified eddy viscosity. It can be calcuated from turbulent intensity and turbulent length scale. "A convenient option is set nuTilda = 5*nut". 2. Can you share your answer? 3. I am not understand what you want simulate. A fixed valued inlet velocity can not meet your standard? I mean why velocity need to accelerate suddenly to generate votices? And what is your net circulation ? |
|
Tags |
nut nutilda, spalart allamaras |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Spalart and Allmaras Paper | Mohamed | Main CFD Forum | 7 | July 10, 2014 17:39 |
CFX Spalart Allmaras turbulence models | aweizazuji | CFX | 9 | September 24, 2013 11:53 |
Spalart Allmaras Paper | Seroga | Main CFD Forum | 0 | April 7, 2008 03:48 |
spalart allmaras paper | hafiz | Main CFD Forum | 1 | April 10, 2007 04:47 |
extracting K and Epsilon from Spalart Allmaras | Sundar | Main CFD Forum | 4 | July 31, 2006 03:02 |