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 realanony87 June 1, 2009 09:31

Turbulent length scale setting

Hello,
How would setting the values for k and the turbulence length scale for the SST turbulence model effect the convergence of a problem ? As I understand the length scale is used to calculate epsilon at the inlet. However if the problem to be solved is a flow over a wing , and the wing is far several chord lengths away from the inlet, I find in contour plots that the kinetic turbulent energy decreases rapidly after the inlet. So what difference does it actually make if I set the turbulence length scale to be the thickness of the wing or the thickness of the boundary layer ?
Thanks

 ghorrocks June 1, 2009 18:40

Hi,

The k or turbulence intensity comes from the turbulence levels. Often for airfoil experiments that is just defined as a turbulence percentage. It is a bit trickier for the second turbulence variable as there is no simple measurement which can define it. So often people just guess a length scale and use the e value which comes from that.

This can lead to an over-estimate of e. As e is the turbulence dissipation this will then eat up the turbulence level at the inlet until it establishes a new equilibrium between turbulence creation (through shear and other mechanisms) and destruction (through e, turbulence dissipation). That is why you see a rapid reduction in turbulence levels near the inlet.

If you see this and you know your turbulence intensity is correct at the inlet, this means the turbulence intensity after the e has established equilibrium is wrong. You had too much e and should reduce it until the turbulence value a distance away from the inlet (when equilibrium between turbulence creation and destruction is established) matches the turbulence intensity you need.

Glenn Horrocks

 realanony87 June 1, 2009 20:31

Hey Glenn, Thanks.
"If you see this and you know your turbulence intensity is correct at the inlet, this means the turbulence intensity after the e has established equilibrium is wrong. You had too much e and should reduce it until the turbulence value a distance away from the inlet (when equilibrium between turbulence creation and destruction is established) matches the turbulence intensity you need."

I am supposed to set the turbulence dissipation e so that I get the turbulence level I want at the wing. However this means that to decrease e, I have to increase the turbulence length scale, which doesn't make sense for me. Shouldn't I be worried about modelling the dissipation in the region of flow over a body itself ?

From the simple relation e= C k^(3/2)/l , decreasing e means increasing the length scale. This may mean that the length scale many times larger than the wing itself if I have a large inlet region and want to have a 1% turbulence level at the wing. Is this a limitation of the turbulence modell that I have to deal with ?

 ghorrocks June 2, 2009 00:58

Hi,

What do you mean "modelling the dissipation in the region of flow over a body itself"?

I don't see the significance of the turbulence length scale to your airfoil. I see no reason why the incoming turbulence could not have a length scale larger than the wing. That is why aircraft go bump when they fly through turbulence.

But your final comment is correct as well - The simple 2-equation turbulence models may not be appropriate. That is up to you to determine.

Glenn Horrocks

 Bollonga October 14, 2012 13:29

Quote:
 Originally Posted by ghorrocks (Post 217840) This can lead to an over-estimate of e. As e is the turbulence dissipation this will then eat up the turbulence level at the inlet until it establishes a new equilibrium between turbulence creation (through shear and other mechanisms) and destruction (through e, turbulence dissipation). That is why you see a rapid reduction in turbulence levels near the inlet. If you see this and you know your turbulence intensity is correct at the inlet, this means the turbulence intensity after the e has established equilibrium is wrong. You had too much e and should reduce it until the turbulence value a distance away from the inlet (when equilibrium between turbulence creation and destruction is established) matches the turbulence intensity you need. Glenn Horrocks
Hi Glenn,

In my case I have a 2D inclined flat plate at high angle of attack, 70º. I have 10 m/s and 10% Iu at the inlet. I am using 0.05 m length scale, and I am getting Iu reduced to 0.1% at some distance away from the inlet. I am also facing viscosity ratio limitation to 1e5 in some cells in the wake of the plate.

Should I use a bigger length scale so ephsilon will be lower and the Iu won't be reduced that much? Wouldn't that make my viscosity ratio even bigger so I'll get it limitated in more cells?