|
[Sponsors] |
Two-phase critical flow and shock modelling of nozzle |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
December 4, 2014, 10:12 |
Two-phase critical flow and shock modelling of nozzle
|
#1 |
Member
Jógvan
Join Date: Feb 2014
Posts: 32
Rep Power: 12 |
Hi.
I am trying to use the experiments from an article in order to validate two-phase critical flow and shocks for water-air in STAR-CCM+. (Sadly, the article is behind a payment wall). The geometry and boundary conditions can be seen in the image below: The air inlet has a pressure of 6 bar and the outlet has pressure of 2.44 bar. The mass flow rate of water is fixed at 498 kg/h. I am using the Eulerian multiphase segregated flow solver with both water and air set to be compressible. I have been able to obtain reasonable results for the critical mass flow rate, but it has not be the case for the pressure profile along the nozzle as STAR-CCM+ does seem to over-predict the shock. As of now, I have been using the S-gamma model in order to describe the interaction length scale for the two-phases by the Sauter Mean Diameter as recommended in the user guide (for droplets/bobbles). My issue is though that I don’t know if this model is applicable for my case? It is also possible to set the interaction length scale to a constant, but I am hoping to avoid this as it will make it troublesome to transfer the validation case to a real case. Or is there a way to calculate the interaction length scale base on physical properties ? Any help would be greatly appreciated. - Jeggi |
|
Tags |
critical mass flow rate, s-gamma, shock, two-phase |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Different flow patterns in CFX and Fluent | avi@lpsc | FLUENT | 4 | April 8, 2012 07:12 |
Con-Div Nozzle Shock structure problem | padmanathan | FLUENT | 2 | November 16, 2010 04:37 |
Nozzle flow simulation in inviscid and viscous | Cath | FLUENT | 0 | January 28, 2007 03:16 |
Nozzle Flow with shock | jim clancy | FLUENT | 1 | December 18, 2001 05:19 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 13:19 |