|
[Sponsors] |
![]() |
![]() |
#1 |
New Member
Join Date: Mar 2009
Posts: 24
Rep Power: 16 ![]() |
in my domain, there is a internal flow exit boundary, which has a supersonic mach number, approximately 1 to 2, and also a fixed mfr (very high obviously). I am just wondering how can i set the boundary conditions in CFx12
|
|
![]() |
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Wind turbine simulation | Saturn | CFX | 58 | July 3, 2020 01:13 |
mass flow in is not equal to mass flow out | saii | CFX | 12 | March 19, 2018 05:21 |
back pressure at exit for supersonic flow | BigFrank | FLUENT | 6 | April 24, 2014 15:13 |
about boundary condtition for exit | luckyluke | FLUENT | 1 | November 30, 2004 09:36 |
Boundary layers in supersonic flow | bob Will | Main CFD Forum | 4 | April 23, 2000 23:19 |