Rocket thrust chamber - Doublet Impingement -- CFD Online Discussion Forums

December 16, 2017, 01:20	Rocket thrust chamber - Doublet Impingement	#1
Goky New Member Gokul V Join Date: Sep 2017 Posts: 4 Rep Power: 9	Hi friends. I am trying to simulate flow field in rocket thrust chamber. I could not find a way to inject gaseous fuel and liquid oxidizer in unlike doublet configuration in fluent. Kindly help me out with your suggestion. Thank you Last edited by Goky; December 16, 2017 at 02:29.

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
Thrust vectoring of rocket nozzle by a jet tab	umesh k.	Fluent Multiphase	0	January 17, 2017 08:33
combustion flow simulation in liquid rocket thrust chamber	geetha sri	FLUENT	1	February 4, 2016 18:04
Flow analysis from a pressurised chamber to a larger chamber	WT4	Main CFD Forum	3	November 4, 2015 23:19
Calculating thrust for a rocket nozzle for a biphasic fluid	toniatop	CFX	0	January 17, 2013 20:15
urgent-reacting flow modelling in thrust chamber	eshwar	FLUENT	2	March 24, 2005 06:01

All times are GMT -4. The time now is 20:08.