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

Estimation of TKE from RANS analysis of Compressible flow with Spalart-Allmaras model

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   January 30, 2024, 14:15
Default Estimation of TKE from RANS analysis of Compressible flow with Spalart-Allmaras model
  #1
New Member
 
Dónal McCaughey
Join Date: Sep 2021
Posts: 9
Rep Power: 4
Dónal is on a distinguished road
I'm trying to estimate the TKE from RANS results of a compressible flow with the Spalart-Allmaras turbulence model. I am familiar with the estimation used in OpenFoam from Bourgoin, but this estimation is based on relationships from P Bradshaw, DH Ferriss, and NP Atwell. Calculation of boundary-layer development using the turbulent energy equation. Journal of Fluid Mechanics, which are for incompressible flow.

I am trying to come up with an estimate based on the Boussinesq hypothesis but I'm confused by the notation of the final term in the brackets. for say the xx Reynolds stress, the first term in the brackets will become 2 * par U / par X. The other term in brackets has the subscript k, so I'm not sure if it becomes the sum of the Y and Z normal strains (the ones that aren't i or j), or if it's the sum of all three components (X,Y and Z)
Attached Images
File Type: png 2be4af261a0a8bfb803a0a2f0f4b3eb1.png (2.6 KB, 8 views)
Dónal is offline   Reply With Quote

Old   January 30, 2024, 17:24
Default
  #2
Senior Member
 
NotOverUnderated's Avatar
 
ONESP-RO
Join Date: Feb 2021
Location: Somwhere on Planet Earth
Posts: 127
Rep Power: 5
NotOverUnderated is on a distinguished road
The second term inside brackets is the divergence of U. The repeated index k implies summation (a.k.a Einstein notation):

\frac{2}{3}\frac{\partial U_k}{\partial x_k}\delta_{ij} = \frac{2}{3}\left(\frac{\partial U_1}{\partial x_1} + \frac{\partial U_2}{\partial x_2} + \frac{\partial U_3}{\partial x_3} \right)\delta_{ij} = \frac{2}{3}\mathrm{div}(\vec U) \delta_{ij}
__________________
Don't keep making the same mistakes. Try to make new mistakes.
NotOverUnderated is offline   Reply With Quote

Reply

Tags
boussinesq, compressible, reynolds stresses, turbulence, turbulent kinetic energy


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Wind tunnel flow simulation boundary condition issue charan3007 SU2 0 October 21, 2021 08:27
Implementing compressible turbulence model in incompressible flow solver CFDanielGER OpenFOAM Running, Solving & CFD 0 March 4, 2021 07:21
parallel code samiam1000 SU2 3 March 25, 2013 04:55
Numerical integration of Spalart Allmaras turbulence model RenardP Main CFD Forum 0 June 11, 2009 14:53
Spalart Allmaras Turbulence model - Need article! CFD Student Main CFD Forum 0 December 27, 2004 04:28


All times are GMT -4. The time now is 00:37.