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April 20, 2022, 05:22 |
Finding Transition point over blimp
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#1 |
New Member
Dawn
Join Date: Apr 2022
Posts: 2
Rep Power: 0 |
Hi everyone,
I am relatively new to CFD and I am trying to find the point in which the flow over an blimp transitions from Laminar to Turbulent. I am using the k-omega SST model, and I plotted a contour of the Reynolds using a definition "(density * 20 * x)/viscosity-lam" where 20 ms-1 is the inlet velocity. Unfortunately, it is showing that the Reynolds at the nose -1.27 million Reynolds and the end of the blimp -205k. I tried plotting velocity profiles but it is showing that the flow is going from turbulent to laminar. Cell quality is good, I have 25 boundary layers where y+ < 1. I am not too sure what I am doing wrong, I have searched around and could not find anything helpful to solve the issues I am having. Last edited by Light014; April 20, 2022 at 05:23. Reason: Delete Unecessary Words |
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April 21, 2022, 03:52 |
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#2 |
Senior Member
Alexander
Join Date: Apr 2013
Posts: 2,363
Rep Power: 34 |
you may look for intermittency factor in fluent, It shows transition explicitly
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April 27, 2022, 14:14 |
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#3 |
New Member
Dawn
Join Date: Apr 2022
Posts: 2
Rep Power: 0 |
Ah thank you, when plotting the intermittency contour it shows me where transition occurs. I am trying to plot velocity profiles to prove mesh convergence. Since my boundary layer behaves at an angle, i cannot use the z coordinate to plot my velocity profile. is there a way to create a coordinate axis that is normal to the surface using either cfd post or tecplot?
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