Hi Junting,

I tried running the case and it appears to be very difficult (nearly impossible) to convergence properly. I think the main reason is that you have specified your front and back back boundaries (top and bottom) as slip-wall.

[soln-bcs-top]
type = slp-wall

[soln-bcs-bottom]
type = slp-wall

I'm pretty sure that using a periodic z-direction would help significantly and allow you to drive the pseudo-residuals down several orders of magnitude. Please see Arvind's response in

https://groups.google.com/forum/#!topic/pyfrmailinglist/JLhiy8TV9xo

In summary, you just need name your top and bottom boundary-fields as

"periodic_0_l" and "periodic_0_r"

in you .msh / cgns file, and PyFR builds the connectivity during the import step. In the .ini file you don't have to specify anything.

Cheers,
Niki

On 16/07/19 22:21, Junting Chen wrote:
Thanks Niki, good to know! I understand.

We are running a simple case where the geometry is just a bluff body. Only criteria that we are using to do validation in this case are Strouhal number (shedding frequency), drag and lift. We noticed that increasing dt/pseudo-dt to ~100 can still maintain stability but requiring a bit more niters to let residual drop to a desirable level (equivalent to having dt/pseudo-dt = 30 and niter =20). As far as i understand, the consequence of larger dt/pseudo-dt ratio is more pseudo-steps are required to converge within a physical step, correct me if I am wrong. Also noticed that high residual will lead to wrong result (off shedding frequency).

It would be really nice of you if you can take a look at my setup. I first found out highest value of pseudo-dt I can use is 2.5E-5. Then I slightly pushed dt to 3E-3 trying to find out the boundary where the simulation either breaks or spits out wrong result.

In fact, another feature we are really hoping to see in the next few release is a portal that allows users to implement a specific velocity profile at a boundary. By saying that, another critical test case of ours requires using a time-varying velocity profile at the inlet (so basically we have a bunch of velocity profiles to be implemented at each every time step).

Thanks a lot again for the clarification!

Junting Chen






On Tuesday, July 16, 2019 at 1:38:10 PM UTC-4, Niki Loppi wrote:

    Hi Junting,

    High memory footprint is not the only issue. Construction of the
    global linear system for high-order polynomials is very expensive
    on modern hardware (high memory requirements with low arithmetic
    intensity). Also solving the linear system is challenging due to
    global communications.

    You can read about implicit time-stepping on GPUs from

    
http://aero-comlab.stanford.edu/Papers/Dissertation_Jerry_Watkins-augmented.pdf
    
<http://aero-comlab.stanford.edu/Papers/Dissertation_Jerry_Watkins-augmented.pdf>

    We are working on local implicit (pseudo) time stepping
    approaches, but I'm afraid they won't be ready for the next release.

    Regarding the dt/pseudo-dt ratio, I suggest keeping it in the
    range of 20-50. You can send me your case files if you want me to
    try it.

    Thanks,
    Niki

    On 15/07/19 22:30, Junting Chen wrote:
    Hello,

    Any work ongoing to make the computation in pseudo time steps
    implicit?

    As Niki mentioned, implicit pseudo time stepper caused storage
    issues (in one of the posts). Any chance an implicit option can
    be offered in the next release? Explicit forces pseudo dt being
    extremely small therefore physical dt kind of small even though
    physical time stepper is implicit. I am working on a bluff body
    problem. Aiming to reduce the number of physical time steps
    within a vortex shedding cycle to be around than 20, while now it
    has to be more than 300 to maintain stability.

    Thanks!

    Junting Chen
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