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Getting CFD Nusselt No to correlate with gnielinski theory

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Old   January 28, 2018, 11:14
Post IMPORTANT PLEASE HELP!! Getting CFD Nusselt No to correlate with gnielinski theory
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Jonathan
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Hi there

I am working on a project which is modelling smooth flow through a rectangular micro-channel. (The project does go further but for now this where I need help).

I am trying to obtain a Nusselt number that correlates with the use of Gnielinski theory but thus far I have had little success. I am trying to find htc by doing q/(Twall-Tbulk) but I don’t understand at what point I should take the temps and how I should. I have entered a heat flux BC.

I am using k omega SST model. I am using ANSYS fluent and their post.

If anymore info is needed just ask

Last edited by jonheb; January 28, 2018 at 15:02. Reason: recieved no answers
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Old   February 16, 2018, 20:33
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Rahul
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For example, if you want to calculate Nusselt number at a surface, you need to find Twall- max temp at that point in a surface and Tmean-Avg temp at the surface

You can use your temperature contour to estimate at which point max temp occurs.Later, in CFD post you can create a point by specifying the co-ordinates of that point.
Then create a expression
maxVal(Temperature)@Location(in our case specify the point)

For mean temperature,
areaAve(Temperature)@Location(in our case specify the surface)

Cheers!
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Old   March 2, 2018, 11:23
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Jonathan
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Hey there

I'm trying to get Nusselt for in the centre of the channel flow.

In Fluent I have been drawing a line across the wall and using surface integrals, area weighted average, wall temp for Tw

and then for the Tb I go into post and draw a plane at the same location of the line from above and then areaave temp plane.

I have a constant heat flux of 50000

The problem is these results aren't even close to what the Gnielinski correlation says I should be getting.
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