> How small is the dt that you are using, and do the numbers change when you
> reduce it further?
>
The time step dt = 0.001 when decreased to 5e-4 and even 1e-4 the change in
error is no more 1%

pseudo-niters-max = 50 , using p-multigrid with vermiere pseudo integration
I tried local-pi but it was either unstable or ineffective perhaps I need
to do needs some fine-tuning of my chosen parameters


> What do you mean quantitatively by ‘killing performance’
> Are you using local pseudo dt and PMG etc. for the inner iterations, or
> just plain RK4?
>

As for the matter of performance, using p-multigrid with pseudo-niters-max
of 50 yields a wall clock time of 6 hours if dt is taken as low as 1e-4 for
8x8 mesh to run only 1s ( GPU utilization at less than 15%)

Can you send plots of how the pseudo residuals are converging in each dt?
>
As for the residuals:
p : 5e-5 ~ 1e-4
uv: 1e-6 ~ 1e-7
For reference, the residual history data and the corresponding ini file can
be downloaded from the following link
https://mega.nz/folder/jVZBwIBb#gk6J1zSTM-Hg8GgRzDYysw
I included residual history for 0.25s only

On Wed, Oct 7, 2020 at 22:21 Vincent, Peter E <[email protected]>
wrote:

> So it looks like errors saturate at 8x8 and don’t go down.
>
> So maybe due to the time integration?
>
> How small is the dt that you are using, and do the numbers change when you
> reduce it further?
>
> Regarding:
>
> I tried different zeta values, different pseudo-dt,, more
>> pseudo-niters-max going as high as 50 which is killing my performance
>>
>>
> Can you send plots of how the pseudo residuals are converging in each dt?
>
> What do you mean quantitatively by ‘killing performance’
>
> Are you using local pseudo dt and PMG etc. for the inner iterations, or
> just plain RK4?
>
> Thanks
>
> Peter
>
> Professor of Computational Fluid Dynamics and EPSRC Fellow
> Department of Aeronautics
> Imperial College London
> South Kensington
> London
> SW7 2AZ
> UK
>
>
>
>
>
>
>
> On 7 Oct 2020, at 04:27, Mohamed M. Kamra <[email protected]>
> wrote:
>
> When solver solver.order = 4
> 4x4 : Mesh DOFs = 400
> Variable: U Error L1Norm = 0.000114383
> Variable: U Error L2Norm = 0.000132731
> 8x8 : Mesh DOFs = 1600
> Variable: U Error L1Norm = 3.8896e-05
> Variable: U Error L2Norm = 4.86379e-05
> 16x16 : Mesh DOFs = 6400
> Variable: U Error L1Norm = 3.90541e-05
> Variable: U Error L2Norm = 4.82179e-05
> 32x32 : Mesh DOFs = 25600
> Variable: U Error L1Norm = 3.91447e-05
> Variable: U Error L2Norm = 4.81805e-05
>
> Between the first two meshes, it is not even second order, after the order
> becomes almost 0!
> Vvisualizing the error shows high error everywhere, specifically at high
> gradient areas
> <image.png>
> Error distribution of U for Mesh 16x16 , order 4.0
>
> <image.png>
> Distribution of U Numerical solution for Mesh 16x16 , order 4.0
>
> <image.png>
> Distribution of U Exact solution for Mesh 16x16 , order 4.0
>
>
>
> On Wed, Oct 7, 2020 at 11:28 AM Vincent, Peter E <[email protected]>
> wrote:
>
>> So what orders of accuracy do you get?
>>
>> Peter
>>
>> Professor of Computational Fluid Dynamics and EPSRC Fellow
>> Department of Aeronautics
>> Imperial College London
>> South Kensington
>> London
>> SW7 2AZ
>> UK
>>
>>
>>
>>
>>
>>
>>
>> On 7 Oct 2020, at 03:23, Mohamed M. Kamra <[email protected]>
>> wrote:
>>
>> Hi Peter,
>> You're right. I left the source term in the ini file because it may not
>> evaluate to zero depending on the choice of the length scale in the
>> Reynolds number (since the domain is not a unit square). When the length
>> scale is chosen to be 1 ( Re = 1/nu) which is the case in all of our
>> simulations so far, then the source term vanishes and that's  what's used
>> in the ini file attached.
>> So I don't think that the source term is the cause of the problem. I
>> removed it now just in case but I got the exact same results.
>>
>> Regards,
>> Mohamed Kamra
>>
>> On Wed, Oct 7, 2020 at 10:48 AM Vincent, Peter E <
>> [email protected]> wrote:
>>
>>> Hi Mohamed,
>>>
>>> I am a little confused as to the test case you are using.
>>>
>>> The 2D TGV case in the paper you reference does not seem to use a method
>>> of manufactured solutions, it just solves the regular NS equations without
>>> a source term?
>>>
>>> Apologies if I missed something.
>>>
>>> Peter
>>>
>>> Professor of Computational Fluid Dynamics and EPSRC Fellow
>>> Department of Aeronautics
>>> Imperial College London
>>> South Kensington
>>> London
>>> SW7 2AZ
>>> UK
>>>
>>>
>>> On 6 Oct 2020, at 16:38, Mohamed M. Kamra <[email protected]>
>>> wrote:
>>>
>>>
>>> Hi,
>>> Thanks for the prompt response
>>> I followed the case illustrated in Cox et al article
>>>
>>> https://www.sciencedirect.com/science/article/pii/S0021999116001686?casa_token=Vpk3uWyaxE0AAAAA:IGLI-wLZFaIwfIIOyPM1OZH6-TphsFXG3nTrgAbaSuJkzNJrUbAYDcL-qc9R1WINd9qGIA
>>> It is a double periodic 2D manufactured solution case, the u, v source
>>> terms are evaluated using Mathematica
>>> I attach the ini file here
>>> The Re = 10
>>> I calculated the order of accuracy in the manner described in the
>>> article which is fairly straightforward
>>> <image.png>
>>> <image.png>
>>> where eps_k is the difference between the exact solution and the
>>> numerical solution.
>>> I used the same meshes resolutions as the article 4x4, 8x8, 16x16, 32x32
>>> with double periodic bcs generated using gmsh
>>>
>>> For now, I am only trying to verify the spatial accuracy so following
>>> the article's example I am using very small dt
>>> I tried different zeta values, different pseudo-dt,, more
>>> pseudo-niters-max going as high as 50 which is killing my performance
>>> the only part I did not mess with is the LDG  beta and tau
>>> I double-checked the source terms several times but it seems okay
>>> So I am not sure what could be the problem.
>>>
>>> Appreciate your help.
>>> M Kamra
>>>
>>>
>>>
>>> On Tue, Oct 6, 2020 at 23:51 Vincent, Peter E <[email protected]>
>>> wrote:
>>>
>>>> Hi M Karma,
>>>>
>>>> Could you provide more details of the test case, the way your are
>>>> obtaining the order of accuracy, and the results that you are getting.
>>>>
>>>> Thanks
>>>>
>>>> Peter
>>>>
>>>> Professor of Computational Fluid Dynamics and EPSRC Fellow
>>>> Department of Aeronautics
>>>> Imperial College London
>>>> South Kensington
>>>> London
>>>> SW7 2AZ
>>>> UK
>>>>
>>>>
>>>>
>>>>
>>>>
>>>>
>>>>
>>>> On 6 Oct 2020, at 15:47, mkamra <[email protected]> wrote:
>>>>
>>>> Hello Everyone,
>>>>
>>>> I have a question regarding the order of accuracy of the ACM method;
>>>> Have you done any tests using the method of manufactured solutions (
>>>> published or otherwise) ?
>>>>
>>>> I tried the 2D taylor green benchmark but the order of accuracy I am
>>>> getting is nowhere near what it should be. When comparing with exact
>>>> solution I used the solution points directly not the subdivided solution in
>>>> the vtu file to avoid interpolation issues polluting the order of accuracy
>>>>
>>>> Also regarding the ACM, how would one obtain the residual of the
>>>> continuity and momentum equations? Pseudo-stats only report the change
>>>> between two consecutive pseudo iterations
>>>>
>>>>
>>>> Regards,
>>>>
>>>> M Kamra
>>>>
>>>>
>>>>
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>>>> .
>>>>
>>>>
>>>>
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>>> .
>>> <tg2d.ini>
>>>
>>>
>>>
>>
>

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