|
[Sponsors] |
March 10, 2016, 12:52 |
Hybrid rocket - which solver for combustion
|
#1 |
New Member
.
Join Date: Mar 2016
Posts: 4
Rep Power: 10 |
Hi All!
I want to simulate a combustion in hybrid rocket engine. There will be a injection of liquid kerosene (the fuel injector must be directly modelled, as for example in sprayFoam->sprayCloudProperties) and gaseous oxygen. Which solver should I use and why? I'm thinking about sprayFoam or reactingParcelFoam, but i don't really understand what is the difference between them and if I can model a injector in the latter. Maybe some other solver would be better? Best regards EDIT: It turns out that sprayFoam uses particle tracking which does not support 2D geometries (empty and wedge boundaries). Can anybody recommend any other solver which supports 2D and axisymmetric geometries, liquid and gaseous mixtures, injector modelling and combustion? |
|
Tags |
combustion, hybrid rocket, injector, solver |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
SU2 development for combustion in Hybrid Rocket Motors | rdbisme | SU2 | 0 | November 12, 2015 15:43 |
thobois class engineTopoChangerMesh error | Peter_600 | OpenFOAM | 4 | August 2, 2014 10:52 |
hybrid rocket combustion? | PattiMichelle | OpenFOAM | 0 | November 5, 2009 12:33 |
why the solver reject it? Anyone with experience? | bearcat | CFX | 6 | April 28, 2008 15:08 |
Error during Solver | cfd guy | CFX | 4 | May 8, 2001 07:04 |