Help with 2D supersonic impinging nozzle!!!! -- CFD Online Discussion Forums

February 27, 2006, 17:50	Help with 2D supersonic impinging nozzle!!!!	#1
James Guest Posts: n/a	Hi, I'm modelling a small 2D supersonic nozzle with flow impinging an infinite plate. Re=500000 Mach 3.5 When solving I am recieving a segmentation error after 580 iritations. Similar models, with impingement distances equal to nozzle exit diameter, have run to 300000+ itr. Current model attempting impingement distances 3 times nozzle exit diameter. Mesh is extremely fine at exit and impingement zone. Let me know if you have any ideas or experience to get this thing going. Cheers James

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
C-D nozzle supersonic jet boundary	Gland	FLUENT	4	May 24, 2012 00:25
A supersonic combustion in a Laval nozzle	argeus	FLUENT	0	March 29, 2010 13:52
SUPERSONIC IMPINGING JET	shuo	Main CFD Forum	0	February 12, 2009 03:56
some questions for supersonic channel nozzle	goldenland	FLUENT	2	November 4, 2007 21:18
compressible flow in a counterflow nozzle	d.vamsidhar	FLUENT	0	November 24, 2005 01:45

All times are GMT -4. The time now is 04:18.