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October 28, 2008, 08:07 |
Log-Law on Boundary Layer using Fluent
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#1 |
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Hello everyone,
I am using Fluent to try to simulate the evolution of a turbulent boundary layer on a flat plate of 30 cm of length with a freestream velocity of 5 m/s (2D-Steady state). The mesh is such as : Dx=1mm and Dy=y+ at the wall I've made a theoritical turbulent boundary profile for the velocity inlet condition. This profil follows the regular laws, as : --> U+=y+ [close to the wall] --> U+=1/0.41*ln(y+)+5 [At the log region] --> The deficient law of Coles farther from the wall I ran some simulations using k-eps model with a wall function until the residuals are small enough (< 10e-8). When I compare the numerical results at several x locations with the log law, it doesn't match at all. Has someone have done something similar ? Thank you ! Seb |
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October 29, 2008, 05:34 |
Re: Log-Law on Boundary Layer using Fluent
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#2 |
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I've done a bit with the log-law.
Remember, Coles' function does not satisfy boundary conditions at the outer edge of the BL. Does that affect your CFD model? Also, Coles' log-law constants are very dodgy. He obtained the values for kappa and B_0 using massaged velocity profile data. Sadly, his values are often still treated as universal constants by noobs. |
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October 29, 2008, 06:07 |
Re: Log-Law on Boundary Layer using Fluent
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#3 |
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Actually I thought that wall functions in the RANS models were made to make the flow to fit the sub-layer law and log-law with the "universal" constants.
At the entrance, my theoritical profile is such U+ = 1/0.41 * ln(y+) + 5 [for 10 < y+ < 60] When I get profiles at some location after the simulations, they all fit in a profile such as : U+ = 1/0.41 * ln(y+) + 0.3 [for 10 < y+ < 30] I was wondering if this was coming from the fact that I am simulating a Low Reynolds boundary layer (Rtheta ~ 600). I made a simulation with a higher velocity (and so a different boundary layer at the entrance) at U=100m/s instead of 5m/s and I found the same results... |
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November 4, 2008, 11:08 |
Re: Log-Law on Boundary Layer using Fluent
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#4 |
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After trying different mesh, different profiles at the velocity inlet and different models I found that the best model to simulate the evolution of a turbulent boundary layer is K-EPS --> Realizable --> Enhanced wall treatment.
Using this, the profile of velocity fits the log law fairly well; Besides, the first cell doesn't have to be too small (> y+) |
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