CFD Online Logo CFD Online URL
Home > Forums > FLUENT

analyse supersonic flow

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

LinkBack Thread Tools Display Modes
Old   February 1, 2011, 05:50
Default analyse supersonic flow
New Member
Komola Das
Join Date: Feb 2011
Location: India
Posts: 1
Rep Power: 0
komola is on a distinguished road
Dear fnds,

To analyze supersonic flow in CD nozzle ( Fluent solver) could you please help me out to set the B.C ? Inlet total pressure and temperature and outflow zero gradient at outlet is known. Is there any provision to set outflow zero gradient at outlet ?

With thanks & Regards
komola 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
back pressure at exit for supersonic flow BigFrank FLUENT 6 April 24, 2014 15:13
Probelm with supersonic exhaust to ambient newj CFX 2 August 9, 2012 18:01
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 04:51
Inviscid Drag at subsonic, subcritical Mach # Axel Rohde Main CFD Forum 1 November 19, 2001 13:19

All times are GMT -4. The time now is 11:10.