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

Supersonic compression-ramp flow

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

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 9, 2009, 14:27
Default Supersonic compression-ramp flow
  #1
New Member
 
Abhishek Kaushal
Join Date: Mar 2009
Posts: 2
Rep Power: 0
Abhishek is on a distinguished road
Hi everyone,
i've been trying to simulate the supersonic ciompression ramp flow on fluent. Although i was able to get the steady(mean) values of the parametes (pressure, etc) right, i'm unable to replicate intermittent pressure signal near the compression corner (shock/BL interation).
till now i've tried using the spalart allmaras model only.

I wonder if anyone here has ever tried it before could help me with this.

thanks
abhishek.
Abhishek is offline   Reply With Quote

Old   April 9, 2009, 15:10
Default
  #2
New Member
 
sophie
Join Date: Apr 2009
Posts: 8
Rep Power: 17
sophie-l is on a distinguished road
Hi
The problem with spalart allmaras is that it is 1 equation so it have big problems to accomodate with high gradients
try using density based solver (in place of pressure based)
sophie-l is offline   Reply With Quote

Old   April 10, 2009, 06:25
Default
  #3
New Member
 
Abhishek Kaushal
Join Date: Mar 2009
Posts: 2
Rep Power: 0
Abhishek is on a distinguished road
hey sophie! thanks for replying. All this time i've been using density based SA model only. i guess RANS would do better! I'll try that now.
Abhishek is offline   Reply With Quote

Old   June 14, 2017, 11:41
Default
  #4
New Member
 
Join Date: Oct 2016
Posts: 3
Rep Power: 9
bharathikvl is on a distinguished road
Quote:
Originally Posted by Abhishek View Post
Hi everyone,
i've been trying to simulate the supersonic ciompression ramp flow on fluent. Although i was able to get the steady(mean) values of the parametes (pressure, etc) right, i'm unable to replicate intermittent pressure signal near the compression corner (shock/BL interation).
till now i've tried using the spalart allmaras model only.

I wonder if anyone here has ever tried it before could help me with this.

thanks
abhishek.
hello sir
please can u help me studying this model,
how you compare/validate this model
please ping me on bharathikvl@gmail.com

thank you
bharathikvl is offline   Reply With Quote

Reply

Tags
boundary layer, interaction, ramp, shock, supersonic

Thread Tools Search this Thread
Search this Thread:

Advanced Search
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 Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
back pressure at exit for supersonic flow BigFrank FLUENT 6 April 24, 2014 15:13
Convergence problem in SUPERSONIC FLOW sridhar FLUENT 0 July 7, 2007 11:16
Boundary Condition at outlet for supersonic flow Benjamin Zachariah FLUENT 4 April 22, 2007 23:47
Modeling Bleed in Supersonic Flow Mohd Yousuf Ali FLUENT 0 March 17, 2007 03:51
Inviscid Drag at subsonic, subcritical Mach # Axel Rohde Main CFD Forum 1 November 19, 2001 12:19


All times are GMT -4. The time now is 16:49.