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#1 |
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Guest
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Hi
I need NACA 0012 lift, drag, pitching moment data for low RE incompressible flow. Thanks |
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#2 |
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Check the AAIA database.
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#3 |
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How low Reynolds number?
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#4 |
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I am looking to benchmark my FSI code for laminar case. So I would be looking for RE=100~1000 because it is easy to reproduce. Moreover I would require some pitching airfoil/hydrofol data as well. Thanks
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#5 |
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Might be tough to find. Look for what has been done at Stanford (Ilan Kroo), they have data for Re = O(1000) Not 0012 but 0008. Still good for verification purposes.
-- Jarmo |
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#6 |
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