CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Running, Solving & CFD

Alphat file in heat transfer case

Register Blogs Community New Posts Updated Threads Search

Like Tree19Likes
  • 19 Post By elegant_v

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 16, 2013, 17:53
Default Alphat file in heat transfer case
  #1
Member
 
yu
Join Date: Nov 2010
Posts: 39
Rep Power: 16
xiyuqiu is on a distinguished road
Hello all,

I am trying to run a turbulent heat transfer in a pipe with k-epsilon model using buoyantBuossieqSimpleFoam. I use the hotroom example to set up my case. I don't know what the Alphat file in the 0 folder from the tutorial. I don't see it got calculated from the fvSolution or fvSchemes files. Would someone help? thank you.

best,

yu
xiyuqiu is offline   Reply With Quote

Old   June 8, 2017, 18:39
Default
  #2
New Member
 
Valerie
Join Date: May 2017
Posts: 1
Rep Power: 0
elegant_v is on a distinguished road
Hi Yu, this is an old question, but I encountered the same one. I'll share the information I found as it might help others.

As mentioned in this thread, you can find the code for alphat calculations in the appropriate file in \src\TurbulenceModels\compressible\turbulentFluidT hermoModels\derivedFvPatchFields\wallFunctions\alp hatWallFunctions.

For in the alphatWallFunction, you'll see something like alphat = rho*nut/Prt, where rho is density, nut is the turbulent kinematic viscosity and Prt is the turbulent Prandtl number.

Relations with conventional variables:
Pr = nu/alpha = (viscous diffusion rate/thermal diffusion rate) = (mu/rho)/alpha
and nu = mu/rho

alpha is conventionally defined as the thermal diffusivity, and from these relations it follows that rho*nu/Pr = rho*alpha. In the model, alphat is then defined as the density*thermal diffusivity.

A unit analysis of this train of thought matches the units in the parameter files where alphat [1 -1 -1 0 0 0 0] and mut [0 2 -1 0 0 0 0].

Last edited by elegant_v; June 8, 2017 at 21:07. Reason: Solved
elegant_v is offline   Reply With Quote

Reply


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
[Other] mesh airfoil NACA0012 anand_30 OpenFOAM Meshing & Mesh Conversion 13 March 7, 2022 18:22
[swak4Foam] Error bulding swak4Foam sfigato OpenFOAM Community Contributions 18 August 22, 2013 13:41
which tutorial can find that include Riemann boundary condition? immortality OpenFOAM Running, Solving & CFD 12 May 3, 2013 19:21
[swak4Foam] funkySetFields compilation error tayo OpenFOAM Community Contributions 39 December 3, 2012 06:18
1.7.x Environment Variables on Linux 10.04 rasma OpenFOAM Installation 9 July 30, 2010 05:43


All times are GMT -4. The time now is 14:30.