|
[Sponsors] |
May 15, 2003, 07:13 |
k-e in laminar flow
|
#1 |
Guest
Posts: n/a
|
Hi.
I was wondering. Can a turbulent model like (eg.) k-e or RSM calculate a laminar flow correctly? If no, what do one do in a case where there are both laminar and turbulent flow zones? Thanks. |
|
May 15, 2003, 08:17 |
Re: k-e in laminar flow
|
#2 |
Guest
Posts: n/a
|
You can't use k-epsilon to do laminar flow. If you have regions of both laminar and turbulent flow then you need a method for predicting the transition point as well as a method of damping the turbulent contributions (so that they are zero in laminar flow). I don't know of any schemes that can do this in general flow configurations. Predicting flow transition is still very much an open problem and is an active area of research.
|
|
May 15, 2003, 10:27 |
Re: k-e in laminar flow
|
#3 |
Guest
Posts: n/a
|
Ok. Thank you for your answer.
|
|
May 16, 2003, 05:21 |
Re: k-e in laminar flow
|
#4 |
Guest
Posts: n/a
|
Some codes can deal with transition alledgedly, but in fact you supply the transition region a priori as far as I understand and the topic of a self-determining transition is indeed an active field of research.
|
|
May 20, 2003, 13:09 |
Re: k-e in laminar flow
|
#5 |
Guest
Posts: n/a
|
The Wilcox book (Turbulence modeling for CFD) gives a good overview of transition modelling with the k-epsilon and k-omega models.
alternatively, try: D.C. Wilcox "Simulation of Transition with a Two-Equation Turbulence Model" AIAA Journal, Vol 32, No. 2, February 1994. this is mainly about the k-omega model but does give a good insight into the problems with two-equation models and transition. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Boundary Layer of Laminar Flow over a Flat Plate | Blasius_Pohlhausen_Crocco | Main CFD Forum | 12 | September 30, 2013 18:35 |
Can I use turbulent model to solve a laminar flow? | nikhil | FLUENT | 5 | February 1, 2011 11:42 |
How to enforce laminar flow while using k-e | Grzegorz Kondora | FLUENT | 0 | January 28, 2009 11:35 |
grid for laminar flow | kim | FLUENT | 2 | April 4, 2002 03:44 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 13:19 |