Mesh in Boundary Layer
Posted: Wed May 08, 2013 7:51 am
Hello,
I have some doubts during my simulation with Code_Saturne.
1) I use k-epsilon model to simulate high reynold number flow in a tube (Re= 7*10^5). The result didn't converge well,the first time step stops at N_iter=N_iter_max =10000(I have already decrease the precision from 10E-08 to 10E-06). And in the listing, it informs me that my mesh is "too refine at the wall,... yplus must be greater than the limit value YPLULI=0.2381E+01". I have an impression that, in the k-eps model the mesh can't be too in the boundary layer, the first mesh should put into the turbulence well developed domain. Is this the reason for the "too refine at the wall" information?
When I enlarge the mesh, the "too refine" information still appear, how should I modify the mesh, I'm confused. I think the LAW OF WALL may help to do the theorical calulation of y+.
Should I do like below:
u_fric=sqrt(tau/rho),
tau is the wall shear stress, tau= mu*(du/dy)|y=0
y+=u_fric*y/nu
Is "y" where I should put my first mesh?
2)When the thermal boundary layer is also involved, how can I define the first mesh?
3)Among the RANS model, which model can allow me see the transient of boudary layer?
Thx a lot!
Luyi
I have some doubts during my simulation with Code_Saturne.
1) I use k-epsilon model to simulate high reynold number flow in a tube (Re= 7*10^5). The result didn't converge well,the first time step stops at N_iter=N_iter_max =10000(I have already decrease the precision from 10E-08 to 10E-06). And in the listing, it informs me that my mesh is "too refine at the wall,... yplus must be greater than the limit value YPLULI=0.2381E+01". I have an impression that, in the k-eps model the mesh can't be too in the boundary layer, the first mesh should put into the turbulence well developed domain. Is this the reason for the "too refine at the wall" information?
When I enlarge the mesh, the "too refine" information still appear, how should I modify the mesh, I'm confused. I think the LAW OF WALL may help to do the theorical calulation of y+.
Should I do like below:
u_fric=sqrt(tau/rho),
tau is the wall shear stress, tau= mu*(du/dy)|y=0
y+=u_fric*y/nu
Is "y" where I should put my first mesh?
2)When the thermal boundary layer is also involved, how can I define the first mesh?
3)Among the RANS model, which model can allow me see the transient of boudary layer?
Thx a lot!
Luyi