|
[Sponsors] |
May 11, 2015, 10:00 |
Static pressure boundary condition
|
#1 |
New Member
Sergio
Join Date: May 2015
Posts: 10
Rep Power: 11 |
Hello,
I am simulating a very basic wind tunnel. I have the mesh done and the solution has converged. I have simulated it with pressure boundary condition. I know that the total pressure increase in the axial fan is 1500 Pa, so the outlet condition is a gauge pressure (static) of 0 Pa and the inlet condition is a gauge pressure (static) of 1500 Pa. But I must give fluent the total gauge pressure (static+dinamic), What can I do it If I donīt know the velocity in the fan outlet? Another problem I have is If I give a total gauge pressure (estimated), the static pressure in that section is non-uniform, but the fan gives an uniform pressure I think. Is this normal? Thank you |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Boundary Condition for pressure and velocity | mecman | OpenFOAM Pre-Processing | 1 | May 7, 2014 17:51 |
Radiation interface | hinca | CFX | 15 | January 26, 2014 18:11 |
Question about heat transfer coefficient setting for CFX | Anna Tian | CFX | 1 | June 16, 2013 07:28 |
An error has occurred in cfx5solve: | volo87 | CFX | 5 | June 14, 2013 18:44 |
how to replace a shock tube high pressure port by a boundary condition? | immortality | OpenFOAM Pre-Processing | 0 | May 2, 2013 14:43 |