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-   -   Stability Problem with sonicFoam for Nozzle Flow (http://www.cfd-online.com/Forums/openfoam/65583-stability-problem-sonicfoam-nozzle-flow.html)

Julian K. June 19, 2009 05:25

Stability Problem with sonicFoam for Nozzle Flow
 
Hi,

I have a stability problem in my flow simulation. Here's the configuration:

I'd like to simulate the flow air through a convergent-divergent nozzle. The geometry starts at the inlet and stops at the outlet of the nozzle. The flow should be critical in the throat. For this I use a pressure difference of dp=300mbar, whereas at the inlet I apply atmospheric pressure. The the calculation I use the sonicFoam solver with 2nd order, bounded interpolation schemes (limitedLinear with phi=1/0.5 and MUSCL) for the divergence terms.


I set the BCs as follows:
/0/p:
Code:

    inlet
    {
        type            totalPressure;
        p0              uniform 1.01325e+05;
        U                U;
        phi              phi;
        rho              none;
        psi              none;
        gamma        1.4;
        value          uniform 1.01325e+05;
    }

    outlet
    {
        type            fixedValue;
        value          uniform 0.71325e+05;
    }

/0/U:
Code:

    inlet
    {
        type            pressureInletVelocity;
        value          uniform (0 0 0);
    }

    outlet
    {
        type            zeroGradient;
    }

    wall
    {
        type            fixedValue;
        value          uniform (0 0 0);
    }

What happens is the following:
The simulation starts fine. The p-, U- and T-fields develop as they should. Shocks occur, which cause a separation of the boundary layer resulting in a creation vortices, which are eventually transported towards the outlet.
However, at some point the solution becomes unstable. At the outlet there is a drastic increase in velocity and pressure (of order > 10^30). Also negative pressure occurs near the outlet. Then the simulation crashes.

I suppose the reason for this effect is the BC at the outlet. What I could do is to fix the pressure, velocity and temperature at the inlet and have 'zeroGradients' at the outlet. However, for my analysis it is necessary to induce the flow via a pressure difference between inlet and outlet.

Julian K. June 19, 2009 08:42

As suggested by prapanj in this thread (http://www.cfd-online.com/Forums/ope...-velocity.html) I used the 'waveTransmissive' BC for the pressure at the outlet. Now, the simulation seem to be stabilized, however it's still running so that, yet, I cannot tell if it works. I hope so ;).

girogirozakk June 29, 2009 19:46

Hi

I try to solve nozzle-flow and my sample-files are opened on my URL.
http://giropenfoam.web.fc2.com/sample/index_sample.html

This is how you can help?

faghat.oo July 2, 2016 04:57

LES sonicFoam
 
Dear Foamers:
I need help in sonicFoam solver. I am working on a project with sonicFoam and an example like shocktube. I have run it with RAS turbulency model but the results have bad errors. I want to solve it with LES but I don't have the related files. who has the below files related to LES shocktube :
1- fvSolution
2- fvSchemes
I need your helps please....

blais.bruno July 11, 2016 08:14

Other than people trying to steal your topic, how did you results end up?

It seems like you had a bad case of a boundary condition polluting your simulations, which happens a lot for compressible flows.


Quote:

Originally Posted by Julian K. (Post 219886)
As suggested by prapanj in this thread (http://www.cfd-online.com/Forums/ope...-velocity.html) I used the 'waveTransmissive' BC for the pressure at the outlet. Now, the simulation seem to be stabilized, however it's still running so that, yet, I cannot tell if it works. I hope so ;).



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