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]<mailto:[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]<mailto:[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]<mailto:[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]<mailto:[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]<mailto:[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]<mailto:[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]<mailto:[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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