I am simulating 2D axial compressor blade in nek5000, using 4 non-periodic and
4 periodic boundaries, respectively (see attachment A).
I am trying to simulate Re=1385. Hence, I did it in 2 separate ways: Case A and
Case B, as mentioned below.
Case A: (Reynolds Number = 1385)
Density = 1, ux=cos42 & uv = sin42 (V=1), characteristic length is set in
mesh as 1, viscosity= -1385. As a result, I am getting the separation of
boundary layer and vortices at the end (see attachment B).
Case B: (Reynolds Number = 1385)
Density = 1, ux=cos42 & uv =
sin42 (V=1), characteristic length is set in mesh as 1, Re=1/1385. As a result,
I am getting the separation of boundary layer but NO vortices at the end as I
got in Case A(see attachment C).
My question are:
Firstly, since Reynolds Number can be specified in both the ways; Case A and Case B and the value of Re is also same .i.e 1385. So why I am getting different results in both the cases????
Secondly, when I am trying to
simulate Re=-138500 with all other values kept as Case A, my solution diverges.
I have tried refining my grid but I still get divergence.
Any help in resolving the above-mentioned problems will be highly appreciated.
Regards.