 |
 |
 |
|
|
|
[Sponsors] | ||||
December 16, 2017, 00:20
|
Rocket thrust chamber - Doublet Impingement
|
#1 |
|
New Member
Gokul V
Join Date: Sep 2017
Posts: 4
Rep Power: 7  |
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. |
|
|
|
|
 |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
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 |
Linear Mode
