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

Effect Reynolds No. on potential core region of 2D JET

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 7, 2023, 13:22
Default Effect Reynolds No. on potential core region of 2D JET
  #1
New Member
 
Muhammad Bilal
Join Date: Aug 2022
Posts: 3
Rep Power: 3
Muhammad Bilal is on a distinguished road
I have done simulation on 2D JET on different Reynolds No from 200 to 5000. My results showed When we increase reynold number its potential core region also increases. why is it so? can anyone tell me?
Muhammad Bilal is offline   Reply With Quote

Old   August 7, 2023, 14:35
Default
  #2
Senior Member
 
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,773
Rep Power: 71
FMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura about
Quote:
Originally Posted by Muhammad Bilal View Post
I have done simulation on 2D JET on different Reynolds No from 200 to 5000. My results showed When we increase reynold number its potential core region also increases. why is it so? can anyone tell me?



What kind of formulation are you using? At higher Re number there is no physical meaning in an unsteady 2D simulation.
FMDenaro is offline   Reply With Quote

Old   August 7, 2023, 16:28
Default
  #3
Senior Member
 
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
Rep Power: 66
LuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura about
The boundary layer gets thinner when all you do is increase the velocity. The same happens on a flat plate.
LuckyTran 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
Ncrit for a glider Xfoil. How to use it. GPT4 answer AlanMattanó Main CFD Forum 0 April 10, 2023 12:16
Simulation of Axisymmetric Free Jet using LRR Reynolds Stress Model skyinventorbt OpenFOAM 1 January 2, 2022 17:42
Error when solving p_rgh bob94 OpenFOAM 0 March 17, 2020 08:12
Simulation of jet at reynolds number 1850 tanmay singhal FLUENT 0 February 24, 2015 10:58
velocity decay and potential core arthur john Main CFD Forum 0 July 14, 2014 02:41


All times are GMT -4. The time now is 21:52.