jet structure at the end of a 2D supersonic nozzle -- CFD Online Discussion Forums

November 7, 2001, 04:05	jet structure at the end of a 2D supersonic nozzle	#1
N Menon Guest Posts: n/a	I'm using CFX TASCflow to model the 2d jet structure at the exit of a supersonic nozzle. Im having convergence problems using a supersonic inlet condition and a supersonic outlet condition to my flow domain. If any one has any prior experiance in a problem of this nature, your sugegstions will be most welcome

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 Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Wind turbine simulation	Saturn	CFX	58	July 3, 2020 01:13
mass flow in is not equal to mass flow out	saii	CFX	12	March 19, 2018 05:21
Water subcooled boiling	Attesz	CFX	7	January 5, 2013 03:32
Constant velocity of the material	Sas	CFX	15	July 13, 2010 08:56
RPM in Wind Turbine	Pankaj	CFX	9	November 23, 2009 04:05

All times are GMT -4. The time now is 14:51.