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

Set initial parameters from Reynolds and Mach number of flat plate

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   June 1, 2016, 22:36
Default Set initial parameters from Reynolds and Mach number of flat plate
  #1
New Member
 
NGUYEN PHAN THAI
Join Date: Aug 2014
Posts: 5
Rep Power: 11
nguyenpt is on a distinguished road
Hello everyone

I'm running test-case of turbulent flat plate[1], and the author only give Re_{\infty}=1x10^6 and Mach_{\infty}=0.1 and not any more.

I need length of flat plate. The author only give it is "c". and I don't know c is 1m or 1cm, or ...? Moreover, I don't know temperature and pressure?...

I'm a new, so, I don't understand more. Can you help me? Thank all you.

--------------
[1] F. Capizzano, Turbulent Wall Model for Immersed Boundary Methods, AIAA, VOL. 49, NO. 11, 2011.
nguyenpt 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
Low Mach number wing/body junction convergence Zen SU2 6 May 3, 2019 04:51
Obtaining Reynolds Number in FLUENT Emmanuel FLUENT 2 April 7, 2016 01:46
Set ONERA M6 Wing Initial Condition Dianhong Main CFD Forum 1 January 20, 2016 05:19
Low mach and reynolds number capability hedley SU2 1 June 5, 2014 15:12
non-dimensional analysis in Fluent Endee FLUENT 8 September 7, 2005 16:16


All times are GMT -4. The time now is 23:35.