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Old   July 8, 2011, 12:50
Default NACA 0012 Experimental Data
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Prasad
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Hello everyone,

I'm looking for experimental pressure coefficient data for the NACA 0012 airfoil to validate simulations that I've run. The Reynolds number is 1e7. Does anyone have any suggestions regarding where I can find such data?

Thanks
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Old   July 11, 2011, 12:34
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f-w
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Have not seen experimental data of 0012 at the high Reynolds number you quote. However, if you are interested in slightly lower Reynolds numbers, you can find references on the following page:
http://turbmodels.larc.nasa.gov/naca0012_val.html
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Old   July 15, 2011, 01:09
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Give me your email addy and i'll send the experimental data to you.

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Old   July 20, 2011, 12:45
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Prasad
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I was able to find suitable data at the link provided. I was also wondering if anyone knew where you could find pressure data for the NACA 0025 airfoil. Everything that I've found so far online mainly is related to lift and drag coefficients.
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Old   February 22, 2016, 03:24
Default Experimental data for NACA 0012
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VEDA MURTHY VEDANTHAM
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vedavvdvvm@gmail.com please can you send the experimental data file to the above mail.
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Old   June 18, 2016, 02:05
Default Help Needed
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Grama Srivatsa
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I'm doing a project on NACA 0012 please send me the experimental data of the air foil
my email id is gramas1996@gmail.com
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Old   June 20, 2016, 02:27
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ByD kevin
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Good day! Prasad, your problem is not very rare, so as what you've said you like to validate the simulations thats why you're looking for experimental pressure coefficient data for the NACA 0012 airfoil, well I'll give you references if you want.
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