|
[Sponsors] |
December 20, 2010, 02:54 |
Boundary layer transition problem
|
#1 |
Member
Edison
Join Date: Mar 2009
Posts: 40
Rep Power: 17 |
I am using DNS to study the boundary layer transition problem. I find in my model, the 3D structures like, lambda vortex, always come up at higher Reynolds number (and correspondingly the waves with higher spanwise wavenumber show weaker amplification), compared with other simulations and experiments.
I am solving 3D vorticity-velocity NS equation with finite difference in downstream and wall-normal directions and spectral method in spanwise direction. I wonder if anyone has similar experience? What are the possible reasons that may lead to current results? Thank you. |
|
December 21, 2010, 13:54 |
|
#2 |
Senior Member
Join Date: Nov 2009
Posts: 411
Rep Power: 20 |
You need to be sure you use the same initial conditions for your simulation as your reference cases. DNS is very sensitive to small modifications of the initial conditions.
Do |
|
December 22, 2010, 01:26 |
|
#3 |
Member
Edison
Join Date: Mar 2009
Posts: 40
Rep Power: 17 |
Thank you so much Do.
Your suggestions inspire me. I measured my initial conditions in spectral space and did not notice the differences with experiments. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[GAMBIT] problems in boundary layer | yubaibai88 | ANSYS Meshing & Geometry | 8 | April 19, 2010 22:07 |
Unsteady Boundary Layer Problem | C.J.Yoon | Main CFD Forum | 0 | January 27, 2006 05:19 |
Wall turbulence, viscosity, boundary layer | Patrick Godon | Main CFD Forum | 1 | November 5, 2003 16:39 |
Boundary Layer Flow Paradox | Wen Long | Main CFD Forum | 3 | September 24, 2002 09:47 |
Modelling Transition in the Boundary Layer | Tara | Siemens | 1 | August 15, 2000 09:49 |