CFD Online Logo CFD Online URL
Home > Forums > Main CFD Forum

reynolds no

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   August 16, 2011, 11:33
Default reynolds no
Join Date: Jul 2010
Location: chennai
Posts: 77
Rep Power: 7
kabilan is on a distinguished road
hai forum
i have airfoil model,velocity,density and viscosity.*vel*x/viscosity...
how can i calculate the reynolds number, i don't know howmuch should i substitute for x value. thanks
kabilan is offline   Reply With Quote

Old   August 16, 2011, 12:20
Join Date: Mar 2009
Posts: 85
Rep Power: 8
husker is on a distinguished road

x is the characteristic length. Here, it is the chord of your airfoil.

Re = Rho * Vel * c / Mhu
husker is offline   Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
New implemented algebraic Reynolds stress model volker OpenFOAM 13 October 21, 2013 00:01
Reynolds Stress Models Jade M Main CFD Forum 0 April 21, 2010 16:38
Reynolds Stress Boundary Conditions tstorm FLUENT 0 July 27, 2009 14:44
Scaling the Reynolds stresses via UDF Markus FLUENT 0 January 23, 2008 06:49
Reynolds stresses without velocity correlations? Phil Main CFD Forum 1 October 2, 2006 04:29

All times are GMT -4. The time now is 15:33.