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

Variation of Turbulent reynolds number Ret with altitude

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 19, 2014, 06:31
Default Variation of Turbulent reynolds number Ret with altitude
  #1
New Member
 
RSS
Join Date: Nov 2011
Posts: 7
Rep Power: 15
rachitsigh11 is on a distinguished road
I am solving k-e turbulence model for normal shock at M=2 at sea level condtions. Now i am doing simulations for different altitudes at 20,40,60 km above sea level in upper atmosphere. I am not able find literature on values of turbulent Reynolds number (ratio of tubulent/eddy viscosity to laminar viscosity) at such high altitudes.


Here is one link regarding turbulent reynolds number.
http://support.esi-cfd.com/esi-users/turb_parameters/


Any comments/suggestions would be helpful. Thankyou.
rachitsigh11 is offline   Reply With Quote

Reply

Tags
atmospheric, euler equations, k-e model, turbulent reynolds number


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
Turbulent viscosity limited to viscosity ratio up to 1e+5 subhas.hunasikatti@gmail. FLUENT 0 January 16, 2014 05:23
hel (turbulent viscosity ratio limited) for supersonic combustion problem omar.2002bh FLUENT 2 September 5, 2012 12:04
pressure eq. "converges" after few time steps maddalena OpenFOAM Running, Solving & CFD 69 July 21, 2011 08:42
Numerical Viscosity - Reynolds Number Ertan Karaismail Main CFD Forum 0 November 20, 2008 18:02
[Commercial meshers] Trimmed cell and embedded refinement mesh conversion issues michele OpenFOAM Meshing & Mesh Conversion 2 July 15, 2005 05:15


All times are GMT -4. The time now is 11:34.