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Hello Zisen, Thank you for reaching out. I'll try to answer you specific questions, but will first circle back on the dt estimate in LMeX.
In practice, I have seen divU-based time step restrictions for low velocity (say Mach < 0.01) cases. If it pops-up on a high velocity case (which your case might be with a CFL dt around 2e-8), it is likely the result of some numerical artifact. Can you give us a bit more details on your case ? If you use hydrogen with pure hydrogen jets, the density of hydrogen is low such that reducing On your specific questions: Cheers, Lucas |
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Hi Lucas and Mark, Sorry for the late update. the problem was solved by reducing cfl from 0.8 to 0.5. As for the peleLM.divu_dt_rhoMin issue, the nominal minimum density in my case is ~0.3 kg /m3, which is near the threshold. thanks, |
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Hello Zisen,
Thank you for reaching out.
I'll try to answer you specific questions, but will first circle back on the dt estimate in LMeX.
There are two main
dt
limits in LMeX: 1) a CFL based and 2) an expansion (ordivU
) based. No Fourier limit since all the viscous terms are solved implicitly.Within the non-subcyling approach of LMeX, the CFL limit will reduce
dt
by a factor two for every new level of refinement (assuming the velocity maximas do not change).The divU-based estimate limits the
dt
based on ~1/divU times how far the density is from a "min" valuepeleLM.divu_dt_rhoMin
, defaulted to 0.1. If the density drops belowpeleLM.divu_dt_rhoMin
, a baseline ~1/divU of dt is used.…