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December 27, 2010, 15:05 |
Not stall
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#1 |
New Member
Join Date: Dec 2010
Posts: 10
Rep Power: 15 |
Hi!
I searched in the entire forum and did not find a precisely answer so i am posting my problem (I'm new in CFX). I'm working with 2D simulation of NACA 0012, with a mesh (unstructured) designed in ICEM. My Cl values seems very good until the stall angle. The cl gets higher and higher while the AOA attack increases. I can see in the post that the separation occured with a streamline, but the cl remains increasing. I used the SST isothermic model. Thanks! |
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December 28, 2010, 04:05 |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Getting accurate models after stall is difficult. You probably won't be able to do it using SST, you will probably need a very careful validated LES/SAS/DES model.
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December 28, 2010, 18:56 |
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#3 |
New Member
Join Date: Dec 2010
Posts: 10
Rep Power: 15 |
Thanks for your answer!
But, what you mean with careful validated ? I tried to use these models and the cl values get close but they remain higher. Do you think it can be related only to my mesh quality? I checked in ICEM and the transition near the airfoil wasn't abrupt, and the quality was good. Thanks again. |
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December 29, 2010, 05:44 |
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#4 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Validated means you have ensured the mesh, convergence, time step and other numerical parameters are correctly set to give the required level of accuracy.
The LES/SAS/DES models will require different time steps and meshes to the RANS models. |
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