Setting the inlet conditions for a scramjet combustor -- CFD Online Discussion Forums

October 14, 2011, 14:37	Setting the inlet conditions for a scramjet combustor	#1
Scramjet2011 New Member Bill Wilson Join Date: Oct 2011 Posts: 1 Rep Power: 0	Question concerning inlet conditions. I am given the following information for a scramjet combustor: stagnation temperature and stagnation pressure of the free stream, and the inlet Mach number. Should a pressure-far-field or pressure inlet be used? If a pressure-far-field inlet can someone help out in setting the gauge static pressure? If a pressure inlet can someone help out in setting the supersonic/initial gauge pressure? Much Thanks.

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
How to set pulsating inlet boundary conditions with a very high frequency	Ton	CFX	10	March 22, 2012 17:57
Setting turbulent plane poiseuille model to periodic boundary conditions.	QBeast	FLUENT	0	July 17, 2011 11:08
pressure with velocity inlet boundary conditions	Ashraf Sharara	FLUENT	1	August 21, 2008 08:29
Setting dynamic pressure as the inlet BC	ruined	FLUENT	1	March 26, 2008 06:30
A problem about setting boundary conditions	lyang	Main CFD Forum	0	September 19, 1999 19:29

All times are GMT -4. The time now is 07:31.