|
[Sponsors] |
April 1, 2010, 01:39 |
sponge layer
|
#1 |
New Member
shuo
Join Date: Apr 2009
Posts: 17
Rep Power: 17 |
Hi
I am reading about using sponge layers as nonreflecting boundary conditions. The implementation appears quite simple. U^(n+1) = U^(n + 1)*(1 - delta) where U is the solution vector and delta is the damping coefficient. The latter varies across the width of the buffer zone. I am wondering whether this B.C. requires a mean flow field as the initial condition. For example, say we want to simulate flow through a nozzle. The inlet conditions are imposed on the left while the rest of domain remains stationary with the sponge included near the nozzle exit. As the simulation begins, isn't the sponge acting as a sink while the flow is moving from left to right? I am a bit confused Regards Shuo |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
NRBC: Sponge layer approach | jinwon park | Main CFD Forum | 1 | December 5, 2013 08:33 |
Trimmer & prism layer | peresah | STAR-CCM+ | 6 | October 6, 2009 15:39 |
Sponge layer for outflow BC | irc | OpenFOAM Running, Solving & CFD | 13 | April 8, 2009 05:18 |
errors | Fahad | Main CFD Forum | 0 | March 23, 2004 14:20 |
Boundary Layer Flow Paradox | Wen Long | Main CFD Forum | 3 | September 24, 2002 09:47 |