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Forum: SU2 Today, 04:00

Replies: 1 SU2 parallel execution fails Views: 164 Posted By sntblm Hello, Did you find any solution? ... Hello, Did you find any solution? Regards.

Forum: SU2 Yesterday, 11:15

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti Thank you very much! I will have a try. . Thank you very much! I will have a try. .

Forum: SU2 Yesterday, 05:45

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By CatarinaGarbacz My first comment is: here you are plotting your... My first comment is: here you are plotting your results, but there is no visual comparison with the reference results, that makes it difficult to say how they compare. If you're discussing a...

Forum: SU2 April 30, 2024, 22:57

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti The thickness I set for the first layer of the... The thickness I set for the first layer of the wall normal element is exactly 1e-7

Forum: SU2 April 30, 2024, 22:54

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti The curves of wall heat flux and pressure look... The curves of wall heat flux and pressure look close, but they are not completely converging, and their peaks are about 5%-6% different. The Ttr cloud picture is close, but the Tve cloud picture...

Forum: SU2 April 30, 2024, 17:59

Replies: 3 help with winglet shape optimisation Views: 67 Posted By bigfootedrockmidget You need to have lower residuals. The adjoint can... You need to have lower residuals. The adjoint can be quite sensitive to left-over errors. I would go to at least 1e-13, preferably 1e-14. You can also see CL still changing so that's an indication...

Forum: SU2 April 30, 2024, 06:39

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By CatarinaGarbacz Hello, slight differences are probably... Hello, slight differences are probably due to the slight differences in the mesh and, potentially, also lack of further convergence. Indeed, near the degree=80-90 on the wall, the convergence...

Forum: SU2 April 30, 2024, 04:27

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti One more question, I saw in your paper that you... One more question, I saw in your paper that you also calculated inviscid flow, how do you give the boundary conditions for inviscid flow? It seems that the wall in NEMO_EULER can only be...

Forum: SU2 April 30, 2024, 04:13

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti What does that mean, please? My understanding is... What does that mean, please? My understanding is that if there are x points circumferential and y points radial, then the total number of grid points is x*y, and the total number of cells is (x-1) *...

Forum: SU2 April 30, 2024, 04:02

Replies: 53 HEG cylinder boundary conditions in NEMO Views: 900 Posted By KleinMoretti Hello, thank you for your help recently！ The... Hello, thank you for your help recently！ The result I got after modifying the 8.0.0 code is very close to the result in your article, but there are still slight differences. Near the degree=80-90 on...

Forum: SU2 April 29, 2024, 17:33

Replies: 3 help with winglet shape optimisation Views: 67 Posted By cfd-jg Thanks for your reply. Yes, I first ran... Thanks for your reply. Yes, I first ran the simulation with MATH_PROBLEM= DIRECT and got a converged result of CL= 0.853490 and CD= 0.011720 99700. So then I used CL = 0.85 as the target lift....

Forum: SU2 April 29, 2024, 16:21

Replies: 3 help with winglet shape optimisation Views: 67 Posted By bigfootedrockmidget The first step is to check the CFD setup. ... The first step is to check the CFD setup. Do you have a fully converged CFD simulation (independent of the adjoint setup) for a specified alpha that shows the expected CL (I guess there is...

Forum: SU2 April 29, 2024, 13:34

Replies: 3 help with winglet shape optimisation Views: 67 Posted By cfd-jg help with winglet shape optimisation Hi all, I am doing my thesis on aerodynamic shape optimisation of winglets. However, I am struggling to make this work on SU2. My aim is to minimize drag maintaining lift fixed. The...

Forum: SU2 April 29, 2024, 05:41

Replies: 3 Restart file question Views: 86 Posted By Athos_e Here are the files. Note how one solution file... Here are the files. Note how one solution file has 0 for Pressure column whereas the other has the correct pressure. For both restart files I get the same results as the picture showing the pressure...

Forum: SU2 April 29, 2024, 05:35

Replies: 3 Restart file question Views: 86 Posted By Athos_e Hello, Thanks for the quick reply. Yeah... Hello, Thanks for the quick reply. Yeah totally makes sense to work like that. But i dont know if I am doing smthn wrong, but i don't think so. I will attach also the files for you to have a look....

Forum: SU2 April 27, 2024, 05:16

Replies: 4 Correct Tipgap Marker? Views: 673 Posted By Tongtong1919 hello , Autogrid is recommended to generate a... hello , Autogrid is recommended to generate a butterfly mesh at the leaf top gap

Forum: SU2 April 27, 2024, 04:27

Replies: 1 Convergence Issue of Rotor67 Simulation under Turbo Mode in SU2 Views: 134 Posted By Tongtong1919 Hi Lin, I looked at the uploaded cfg file and in... Hi Lin, I looked at the uploaded cfg file and in CUSTOM_OUTPUTS, there is an item VELOCITY_ZDENSITY which seems to be used to define the import/export mass flow rate, I would like to ask if...

Forum: SU2 April 26, 2024, 07:18

Replies: 3 Restart file question Views: 86 Posted By bigfootedrockmidget Yes, that is exactly what SU2 does. Note that the... Yes, that is exactly what SU2 does. Note that the filename SU2 uses for restarting is set using : SOLUTION_FILENAME= solution_flow.dat which is by default different from the filename that is used...

Forum: SU2 April 26, 2024, 07:07

Replies: 6 NEMO shock tube with MUTATIONPP Views: 252 Posted By Athos_e Hello again, Sorry for the late reply. Since... Hello again, Sorry for the late reply. Since I last posted on the forum I've read some more papers. I believe the reason my reactions stop is because a reflective wave bouncing of the left wall,...

Forum: SU2 April 26, 2024, 06:59

Replies: 3 Restart file question Views: 86 Posted By Athos_e Restart file question Hello everyone, I have a quick question regarding the restart file in SU2. I am using a .csv file in order to restart a simulation (combining two meshes to form one without using multizone). I...

Forum: SU2 April 25, 2024, 16:04

Replies: 1 Convergence issues with NACA 0012 RANS Test Case Views: 93 Posted By bigfootedrockmidget Could you maybe show how well it does compared to... Could you maybe show how well it does compared to the validation results from NASA: https://turbmodels.larc.nasa.gov/naca0012_val.html They use a very fine grid, and they report results up to a=15

Forum: SU2 April 25, 2024, 16:00

Replies: 7 CGNS Reader cannot handle more than 1 zone? Views: 1,338 Posted By bigfootedrockmidget I think you just have to split the cgns into... I think you just have to split the cgns into separate cgns files for each zone.

Showing results 1 to 22 of 22

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