|
[Sponsors] |
September 5, 2005, 10:20 |
Creeping Flow in CFX
|
#1 |
Guest
Posts: n/a
|
Hello everybody,
I'm simulating the fluid dynamics of steady lubricant flow, which is basically creeping flow governed by the Stokes equations (Re<<1). Is it possible to take the advantage of creeping flow in CFX? In other words, can one cancel some terms in Navier-Stokes equations for a specific simulations? e.g. the convective term. I appreciate any advice/comment on the subject. Best regards. |
|
September 5, 2005, 20:14 |
Re: Creeping Flow in CFX
|
#2 |
Guest
Posts: n/a
|
Hi,
I don't think it is possible to turn the convective terms off. I also suspect you won't have to. For very low Reynolds number flows the simulation should converge very rapidly as the lack of convection makes convergence very easy and fast. Just run it with the convective terms on as normal and it should converge very quickly. Glenn Horrocks |
|
September 6, 2005, 03:44 |
Re: Creeping Flow in CFX
|
#3 |
Guest
Posts: n/a
|
Hi Glenn,
Thanks for your comments. Before I go for the simulations, I also thought as you do: steady creeping flow, no problem, this would converge very rapidly; but it does not. In fact the problem is the ratio of characteristic lengths in respective coordinate directions; e.g. for a journal bearing the ratio of clearance(film thickness) to bearing radius is in the order of 10^-3, i.e. either finite volumes with enormous aspect ratio (poor quality), or models which consists of quite a few million cells (good quality). The number of outer iterations required for convergence is about 150, which I find ridiculous, if I employ a good quality mesh (4.5*10^6 cells),this amount to a huge computational time. The idea was to simplify the Navier Stokes equations in order to have a converged solution after just a few iterations. Wish you all a rapid convergence. Taner Baytekin |
|
September 6, 2005, 20:28 |
Re: Creeping Flow in CFX
|
#4 |
Guest
Posts: n/a
|
Hi,
Are you using CFX4 or CFX5/10? 150 iterations per timestep is not unheard of in CFX4, but CFX5 should have only around 5. The difference in lengths should be OK in either code. A tet/prism mesh in CFX5 will not work well as you say, but a structured (hex) mesh should work well as the flow is aligned with the grid and this greatly mitigates the disadvantages of high aspect ratio elements. Glenn Horrocks |
|
September 7, 2005, 03:30 |
Re: Creeping Flow in CFX
|
#5 |
Guest
Posts: n/a
|
Hi,
I'm using CFX5, the grid should be OK, it is structured hexas and consists of only one block. Another observation is the following: if the aspect ratio of an average hexa is extremely high, about 1:80, then the simulation does not converge, the residuals fluctuates around a constant mean value with rather small amplitudes. Taner Baytekin |
|
September 7, 2005, 19:35 |
Re: Creeping Flow in CFX
|
#6 |
Guest
Posts: n/a
|
Hi,
Have you tried double precision? Glenn Horrocks |
|
September 8, 2005, 03:24 |
Re: Creeping Flow in CFX
|
#7 |
Guest
Posts: n/a
|
Hi Glenn,
I usually use double precision. The problem is now better, I tried the following: I interpolated a coarse grid solution for the initialisation, then the convergenge criteria is fulfilled within 25 outer iterations, I can live with it. Thanks a lot for your comments. Taner Baytekin |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[HELP] Slip flow boundary condtion in CFX | jeffwmb | CFX | 20 | March 13, 2013 17:21 |
Ansys 11.0 CFX - solving electric potentials and multiphase flow | cfd_multiphyiscs | CFX | 2 | March 10, 2010 14:43 |
Different flow pattern between OpenFOAM and CFX | AirS | OpenFOAM | 0 | January 12, 2010 08:08 |
demo free flow blunt body in cfx ansys 11 | jan | CFX | 1 | July 31, 2007 20:44 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 13:19 |