CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > ANSYS > FLUENT

Rocket thrust chamber - Doublet Impingement

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

LinkBack Thread Tools Search this Thread Display Modes
Old   December 16, 2017, 00:20
Default Rocket thrust chamber - Doublet Impingement
New Member
Gokul V
Join Date: Sep 2017
Posts: 4
Rep Power: 7
Goky is on a distinguished road
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 01:29.
Goky is offline   Reply With Quote


Thread Tools Search this Thread
Search this Thread:

Advanced Search
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 Off
Pingbacks are On
Refbacks are On

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 07:33
combustion flow simulation in liquid rocket thrust chamber geetha sri FLUENT 1 February 4, 2016 17:04
Flow analysis from a pressurised chamber to a larger chamber WT4 Main CFD Forum 3 November 4, 2015 22:19
Calculating thrust for a rocket nozzle for a biphasic fluid toniatop CFX 0 January 17, 2013 19:15
urgent-reacting flow modelling in thrust chamber eshwar FLUENT 2 March 24, 2005 05:01

All times are GMT -4. The time now is 02:13.