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April 13, 2009, 12:44
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leading edge separation on airfoil
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New Member
Tenzin Choephel
Join Date: Apr 2009
Posts: 2
Rep Power: 0  |
Hi guys..i want to model the flow over an airfoil using FLUENT for my experimental research project. I am particularly interested in seeing leading edge laminar separation and the ensuing separation bubble and the associated vortex field induced. Is FLUENT capable of doing that?
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April 14, 2009, 12:22
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#2 |
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Senior Member
N/A
Join Date: Mar 2009
Posts: 189
Rep Power: 17 |
If you ensure that you have around 15-20 points inside the boundary layer, you should be able to resolve the LEV.
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April 14, 2009, 23:43
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#3 |
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Member
Join Date: Mar 2009
Posts: 35
Rep Power: 17 |
FLUENT can be used and the boundary layers around the leading edge should be fine enough .
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June 13, 2009, 03:38
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#4 | |
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Member
^_^
Join Date: Mar 2009
Posts: 36
Rep Power: 17 |
How to create the geometry for the leading edge part please? if only the data for pressure side and suction side is available.
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