create a LES inlet
Posted: Wed Oct 14, 2020 10:14 am
Hello,
I have a LES simulation to run. For the inlet, I plan to use the "mapped inlet" function in code_saturne version 6. I'm testing the LES inlet using an isothermal pipe with a length of 10D.
The mesh is generated by extrusion of a 2D plane. I first used k-omega SST to generate a preliminary velocity field. Then the LES is restarted from the result of SST. However, I found the velocity profiles of LES seemed not correct. The boundary layer is thicker compared to the SST result, and the peak velocity in LES is much higher than that in SST. A plot of the velocity profiles are attached. (Vel-SST is the result of SST, Vel-iwallf5 is the LES result with default iwallf=2, Vel-iwallf0 is LES with iwallf = 0).
I haven't figured out why the LES result is so different from the RANS result, and the LES seems to be quite laminar-like although the Reynolds number is around 8600 using the bulk velocity.
Could anyone help have a look at this case to help me out?
Best regards,
Xiaoxue
I have a LES simulation to run. For the inlet, I plan to use the "mapped inlet" function in code_saturne version 6. I'm testing the LES inlet using an isothermal pipe with a length of 10D.
The mesh is generated by extrusion of a 2D plane. I first used k-omega SST to generate a preliminary velocity field. Then the LES is restarted from the result of SST. However, I found the velocity profiles of LES seemed not correct. The boundary layer is thicker compared to the SST result, and the peak velocity in LES is much higher than that in SST. A plot of the velocity profiles are attached. (Vel-SST is the result of SST, Vel-iwallf5 is the LES result with default iwallf=2, Vel-iwallf0 is LES with iwallf = 0).
I haven't figured out why the LES result is so different from the RANS result, and the LES seems to be quite laminar-like although the Reynolds number is around 8600 using the bulk velocity.
Could anyone help have a look at this case to help me out?
Best regards,
Xiaoxue