|
[Sponsors] |
September 30, 2017, 20:26 |
Interfaces Discontinuity
|
#1 |
New Member
Emanuel Camacho
Join Date: Jul 2017
Posts: 8
Rep Power: 9 |
Hi. I'm trying to solve a flapping wing using FLUENT but there's a problem I'm trying to solve for a week! I am using an interface to guarantee that there will not be a reduction in the mesh quality but the interface shows discontinuities in the velocity and pressure fields, as shown in the attached file. I personally think this happens due to mass flow conservation, but is there any way to fix this?
Thanks in advance, Emanuel |
|
October 3, 2017, 16:44 |
|
#2 |
New Member
Emanuel Camacho
Join Date: Jul 2017
Posts: 8
Rep Power: 9 |
Found a solution. Seems that the root's problem was the Transient Formulation. A second order implicit method was making the result unstable. I'm using now the first order implicit with a reduced time step.
|
|
Tags |
fluent, interfaces |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Discontinuity across interfaces | Nurzhan | CFX | 2 | March 11, 2015 02:59 |
What type is defined as the interfaces between stator and stator on OF-2.1.1? | renyun0511 | OpenFOAM Running, Solving & CFD | 3 | May 18, 2013 09:11 |
Discontinuity in interfaces | Lugarin | FLUENT | 0 | July 12, 2011 18:53 |
discontinuity of solution due to interfaces ? | T.D. | OpenFOAM Running, Solving & CFD | 4 | December 20, 2010 10:42 |
grid interfaces | kiko | FLUENT | 0 | February 13, 2007 11:28 |