Hi Neks,
I am simulating flows around a NACA airfoil at Re=10^4/10^6 using the rans_komg.f module from Nek5000 (the latest updated version as reported in the article by Tomboulides et al. Int. J. Heat Fluid Flow 2018). In this regard I have two questions to ask.
The first issue is that when I switch from 2D to 3D with a mesh already used for a DNS, the code after passing inside the fix_geom subroutine reduces my domain in the spanwise direction z. To be precise, the domain in z is equal to one chord (L_z = 1), but "suddenly" it becomes 0.75 with zmin = 0.125 and zmax = 0.875 (while they should be 0 and 1, respectively). Look at the logfile excerpt below ( I have inserted some CHECKS in fix_geom):
...
ywmin and yw 0.6509446E-02 0.6493389E-02 2.000000 8 5 894904
xmin = -19.0000000000000
xmax = 40.0000000000000
ymin = -20.0000000000000
ymax = 20.0000000000000
zmin = 0.000000000000000E+000
zmax = 1.00000000000000
CHECK 01
xmin = -19.0000000000000
xmax = 40.0000000000000
ymin = -20.0000000000000
ymax = 20.0000000000000
zmin = 0.000000000000000E+000
zmax = 1.00000000000000
CHECK 02
xmin = -19.0000000000000
xmax = 40.0000000000000
ymin = -20.0000000000000
ymax = 20.0000000000000
zmin = 0.125000000000000
zmax = 0.875000000000000
7.1054E-15 3.5527E-15 5.0000E-01 7.1054E-15 3.5527E-15 5.0000E-01 xyz repair 1
...
After this, the code gives NaNs (see below...)
...
Dealiasing enabled, nxd= 12
Estimated eigenvalues
EIGAA = 5.85165572031620
EIGGA = NaN
EIGAE = 2.835278483507428E-003
EIGAS = 4.037715447589336E-005
EIGGE = NaN
EIGGS = 2.00000000000000
...
The second problem (more methodological/conceptual) is that the code (for the 2D case, the 3D case does not work as said before) with any turbulence model (in general, uRANS k-omega) provides for long times a steady state even for relatively high angles of attack (alpha=12° and Re=10^6). Which is very strange since I expect at least a global von Kármán-type oscillation.
Thank you in advance for your help.
Best regards,
Gabriele