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Search for cd and cl experimental results of NACA 0012

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Old   April 15, 2012, 16:22
Default Search for cd and cl experimental results of NACA 0012
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spk
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Hi guys,

I search for cl and cd experimental results for airfoil naca 0012 for Re=3.0E06. I have Abbott's book, but i can't distinguish all the points for this Reynolds number, especially for cl.
Please help!!

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Old   April 15, 2012, 20:00
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agd
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Google

http://turbmodels.larc.nasa.gov/naca0012_val.html

First result for a search on "lift coefficient NACA0012 3 million"
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Old   April 16, 2012, 08:49
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Thanks a lot!
I search for accurate experimental data of cl and cd, like a table with the values of cl and cd!
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Old   April 17, 2012, 15:28
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Quote:
Originally Posted by agd View Post
Google

http://turbmodels.larc.nasa.gov/naca0012_val.html

First result for a search on "lift coefficient NACA0012 3 million"
These results are for Re=6E06
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