Jean-François Thomas

Results 5 comments of Jean-François Thomas

I made a light test case to reproduce the issue. It's a cylinder in a flowfield. It's only 112k cells. ![mesh](https://user-images.githubusercontent.com/91184648/145433376-ec7d4309-acc6-43d2-a172-39502e823147.png) ![swpeptCylinder](https://user-images.githubusercontent.com/91184648/145433398-97123613-824f-4f81-a143-aaae790ce252.png) ![residual_energy](https://user-images.githubusercontent.com/91184648/145433426-e6fc38f8-8482-47be-bd52-dca747b3e3e4.png) The residuals never converge: ![residual_convergence](https://user-images.githubusercontent.com/91184648/145432900-0c2d7432-807b-4fe4-b24d-abf01cdc7bc4.png) Here is...

Hi, I tried with SA instead of SA_NEG, I get the same behavior. I understand that I don't need to test the develop branch then. I am ok with some...

Hi @pcarruscag, thank you for the development. I am testing it right now, I already noticed the struggle to converge the linear system. I lowered the CFL and relaxed the...

Hi @pcarruscag, sorry for the delay, I had a week off. I can confirm that it converges now. The only drawback is the longer convergence of the linear system. Thank...

I am referring to the 2.5D wing section.