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November 25, 2017, 13:21 |
Viscous Model
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#1 |
New Member
Felix Issac Arias Alvarez
Join Date: Oct 2017
Posts: 5
Rep Power: 8 |
I am trying to do a flow simulation on my plane. So far i have been using the k-epsilon 2 equations because i saw that on a YouTube video. I am completely new to fluent. I am trying to learn or the terminology.
How do i know which viscous model to use? Do i have to do some hand calculations? I have a delta wing plane with canards at 100 m/s. For mesh i used tetrahedrons, curvature, coarse. My orthogonality quality seems to be 0.099 with a maximum aspect ratio of 30. Thanks for the help. |
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November 29, 2017, 02:20 |
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#2 |
Member
Kirill Borodin
Join Date: Mar 2016
Posts: 60
Rep Power: 10 |
Hello! For such a simulation one should study boundary layer theory. You need a mesh with inflation and prism elements in the boundary layer. How to distribute points in the boundary layer - take y+ value =1 for first layer thickness. For turbulence modeling sst kw is very good, and transition sst can be used for transition modeling (study turbulence and boundary layer theory - you need them)
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December 1, 2017, 20:06 |
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#3 |
New Member
Felix Issac Arias Alvarez
Join Date: Oct 2017
Posts: 5
Rep Power: 8 |
Thanks for the help. I will try to learn boundary layer thickness. I have a fluids books. Do you have any good books as reference to study? I will take your suggestions.
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December 4, 2017, 05:54 |
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#4 |
Member
Kirill Borodin
Join Date: Mar 2016
Posts: 60
Rep Power: 10 |
Hermann Schlichting, Theory of Boundary Layer
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