|
[Sponsors] |
April 4, 2013, 13:57 |
Pressure BC for compressible flow
|
#1 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
Hey lads,
i need an outletInlet bc for pressure in my compressible case,for my farfield. I used outletInlet but it doesn't work. I need something like inletOutletTotalTemperature, which i use for temperature. Anything in mind? I already used totalPressure but it works like fixedValue,i need an outletInlet. Thanks |
|
April 4, 2013, 16:17 |
|
#2 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
use waveTransmissive or now pressureTransmissive i think.there is examples in tutorials.
|
|
April 5, 2013, 06:09 |
|
#3 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
Well, here are my case files.
p GEOM { type zeroGradient; } FARFIELD { type waveTransmissive; value uniform 1e+05; gamma 1.4; phi phi; rho rho; psi psi; lInf 1; fieldInf 1e+05; } T GEOM { type zeroGradient; } FARFIELD { type inletOutletTotalTemperature; U U; phi phi; psi psi; gamma 1.4; T0 uniform 306.534; } U GEOM { type fixedValue; value uniform (0 0 0); } FARFIELD { type pressureInletOutletVelocity; value uniform (100 0 0); } I'm a little stuck here,so thanks for your advise. |
|
April 5, 2013, 13:17 |
|
#4 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
does this settings of BC's work?you could set T also in waveTransmissive form.whats your doubt about?
|
|
April 5, 2013, 13:29 |
|
#5 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
No,they don't work. I want to find the correct combination of those in order for my farfield not to be reflective. I could use something like inletOutletTotalPressure but it doesn't exist. I need something like pressure Farfield in Fluent, which i've seen you are familiar within an other post.
|
|
April 5, 2013, 15:12 |
|
#6 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
in my opinion you should make FarField BC divided into two parts.one for inlet part and one for outlet part.on inlet part you should specify p and T(U be in any kind of zeroGradient BC's) or U and T(p be of zeroGradient kind)
I don't know what do your case and geometry like.do you have an airfoil or something like that? |
|
April 5, 2013, 15:57 |
|
#7 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
I have a sphere geometry in a sphere farfield. What you say sounds great but i will need some guidance in making and applying it.
(Thanks a lot for your interest!) |
|
April 5, 2013, 16:11 |
|
#8 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
oh i remembered you wanted to simulate vortex shedding in a sphere thats in a flow.can't you change farField patch to a cylindrical form that has an inlet and an outlet?
|
|
April 5, 2013, 20:31 |
|
#9 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
Yes,that's me.No, 'cause i've already completed the incompressible simulation and i want the compressible results to have a complete comparison.So,any ideas for the combination of p/T/U at farfield?
|
|
April 5, 2013, 22:16 |
|
#10 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
set T as waveTransmissive as i told you before.if it didn't work set it simply zeroGradien.if this also didn'p work you should set farfield as a cylinder to have certained inflow and outflow patches.do these 3 ones and let me know the results.
|
|
April 6, 2013, 07:51 |
|
#11 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
Ok, but can you explain to me why zeroGradient at farfield? I thought we need something like inlet/outlet or wave transmissive like you've said.
|
|
April 6, 2013, 08:36 |
|
#12 |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 27 |
zeroGradient have to be set for variables that we have to set a value for them for starting numerical calculations and not required by fluid dynamics itself.
inletOutlet is a kind of zeroGradient.when flow is going into domain it has the value we specified ourselves as external value(becomes like fixedValue) and when the flow flows outward! solver read the values of variable in domain and put it on boundary(and becomes zeroGradient). |
|
April 10, 2013, 10:06 |
|
#13 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
A brief report:
the boundary conditions were just fine.The reason why i couldn't see the desired vortices was because rhoCentralFoam is inviscid. I came to this conclusion due to the fact that i get the same and desired distributions of p,T,U with different ( but relative when it comes to their nature) boundary conditions, but i don't see any vortices. So,next step was to change solver. I now use rhoPimpleFoam with laminar simulation, and i can see clearly the desired vortices. The problem know is that the solution crashes after some time, saying something like : Max Number of Iterations Exceeded, which i think is a problem with temperature. Also, i think that the solution is highly dependable from the maxDeltaT and that CFL condition alone is not enough. So,you recommend the same bcs for reaching convergence? |
|
May 19, 2014, 23:03 |
|
#14 |
Senior Member
Daniel
Join Date: Jul 2009
Location: Montreal, Canada
Posts: 156
Rep Power: 17 |
Hello Vasileios,
Could you please expand upon why changing boundary conditions and obtaining the same results suggests that rhoCentralFoam is inviscid? I have been using it to model airfoil flow, and I have found that it does develop a boundary layer and a wake with significant vortices. Maybe something else is wrong with your simulation. I have had different results with rhoPimpleFoam, rhoCentralFoam, and sonicFoam; not sure why, but it seems as though they are suited to different applications. Daniel |
|
May 26, 2014, 13:39 |
|
#15 |
Member
VS
Join Date: Nov 2012
Posts: 86
Rep Power: 13 |
Daniel,
I supposed that rhoCentralFoam is inviscid because, provided that Reynolds is sufficient and the boundary conditions of the farfield do not create numerical reflections that wouldn't allow the flow to separate and the vortices to detach, I came to the hypothesis that this solver solves the Euler formulation of the equations. Kind regards |
|
Tags |
outletinlet, pressurebc, rhocentralfoam |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Pressure Outlet Guage pressure | Mohsin | FLUENT | 36 | April 29, 2016 18:16 |
Non-steady flow simplified for use in Vissim | steamerandy | Main CFD Forum | 0 | October 31, 2011 22:08 |
Pressure outlet in two-phase flow in horizontal 2D channel | AlmostSurelyRob | Main CFD Forum | 0 | November 17, 2010 08:32 |
pressure distribution in water flow, differences in icoFoam and COMSOL | deniggo | OpenFOAM Running, Solving & CFD | 14 | September 30, 2010 04:48 |
Flow not moving - Supersonic/Initial Pressure problem? | shankara.2 | FLUENT | 0 | June 9, 2009 21:49 |