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How to generate acoustic waves in Fluent

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Old   April 3, 2021, 00:26
Default How to generate acoustic waves in Fluent
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Haocheng Yu
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Hi,

I've been trying to simulate the viscous effects on acoustic propagation through a small pipe with infinite length. The challenge is to create acoustic plane waves in Fluent. The user menu suggests that not to use velocity inlet and outflow for compressible flow so I use the pressure inlet and use the expression : P_gauge = sin(2*π*20*t) [Pa] and still not sure how to set the outlet boundary. Any suggestion is appreciated!

Thanks!
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Old   April 3, 2021, 09:26
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You can use a velocity inlet or pressure inlet. I use velocity inlets a lot for acoustic forcing.

For the outlet, use a pressure outlet with the non-reflecting BC option so the waves don't get reflected back.
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Old   April 3, 2021, 16:42
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Haocheng Yu
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Hi Tran,

Thanks for your response. I found the solution of non-reflective pressure outlet does not converge and the residuals goes to infinite after 7 or 8 iterations.

Since the geometry is very simple, I use the automatically generated mesh as attached. Any tips on what way I should go?

I am also not quite sure how to set up the solution method (I tried both implicit and explicit. Neither of them don't work).

Thanks!
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Old   April 4, 2021, 06:02
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Looks like you are running into the typical issue of troubleshooting your very first CFD =)


There is no image that I can see but... It's a pipe... that's one of the simplest geometries to mesh after a box. You don't need anything fancy. A uniform mesh will do for the purpose of propagating acoustic waves. If your mesh is crap of course the simulation will diverge. Now assuming your mesh is decent...

You likely have an initialization problem or something else very trivial wrong in your setup if it diverges that fast. Check your initial conditions and so on. Try running a steady case with a simple constant pressure inlet and pressure outlet and go from there.
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Old   April 5, 2021, 22:48
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Hi Tran,

I think the problem is due to compressibility. I tried the simplest case where the pressure inlet gauge pressure is 0 [Pa] and the non-reflective pressure outlet is 0 [Pa] with steady state. The geometry is a 2D rectangular with uniform mesh and its top and bottom bounded by walls. The solution still diverges quickly. Same is for a 3D axisymmetric pipe.

However, it will converge if I use the pressure-based solver. Do you have any simple case files that I can learn from to make the density-based solver converge?

Thanks!
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