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July 29, 2012, 22:53
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low reynolds number
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#1 |
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New Member
JEEVA J
Join Date: Jul 2012
Posts: 2
Rep Power: 0  |
Hello
I'm having problem in fluent, my CL and CD values are very very low when compared to the experimental results. could anyone help me in this I'm generating flow over Zimmerman Inverse wing,my flow conditions are V=4.1 m/s Re=70000 chord=0.25m I have given following condition in fluent 1.Pressure based solver 2.laminar flow 3.simple solver 4.first order & second order solution BC 5.velocity inlet and outflow boundary condition 6. Wing wall condition 7. surrounding symmetry condition |
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July 30, 2012, 02:32
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#2 |
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New Member
ali
Join Date: Feb 2012
Location: tehran.iran
Posts: 5
Rep Power: 14 |
use K_E model to simulate this flow and compare your Cd &Cl with experimental data
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July 30, 2012, 03:58
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#3 |
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New Member
JEEVA J
Join Date: Jul 2012
Posts: 2
Rep Power: 0 |
thanks for ur but still it's not working
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