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NACA 0012 Experimental Data

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Old   July 8, 2011, 13:50
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, 13:34
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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, 02:09
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Give me your email addy and i'll send the experimental data to you.

Ralph
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Old   July 20, 2011, 13:45
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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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vedavvdvvm@gmail.com please can you send the experimental data file to the above mail.
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Old   June 18, 2016, 03:05
Default Help Needed
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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   December 4, 2016, 01:41
Default validation of incompressible laminar flow solver
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I have written a SIMPLe algorithm flow solver and I should validate my solver for airfoil. My question is that, is there any experimental data for airfoil to validate an incompressible laminar flow solver?
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Old   April 6, 2017, 07:23
Default Experimental data for Naca 0012
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Reuben
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Hey guys,

I have gone onto the website https://turbmodels.larc.nasa.gov/naca0012_val.html and I have looked everywhere. What I need is the lift and drag coefficient of the experimental data for this airfoil, can anyone help?

Last edited by Hulk_25; April 6, 2017 at 07:24. Reason: Clarity
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Old   April 6, 2017, 15:53
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Good luck. There are several conflicting data sets available for this airfoil. You are better off choosing a different profile for validation.
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Old   May 28, 2017, 11:15
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please also send me it
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Old   January 11, 2018, 11:52
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Can you please send it to me as well?

kwagner@mail.hs-ulm.de

Thank you
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Old   March 19, 2018, 10:41
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Could you share with me the data?

Thanks

ebubekir.akarsu@gmail.com
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Old   May 18, 2018, 04:58
Default Experimental data for Naca 0012
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Can you please send it to me as well for Reynold number =3*10^6 ?
dimitrazio@hotmail.gr
Thank you in advance!!
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Old   December 1, 2018, 10:49
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Hello dear Ralph

could you please send me the experimental data of naca0012?

my mail:k.nav1996@gmail.com
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Old   December 27, 2018, 03:31
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Hello dear Ralph

could I get the experimental data of naca0012?

my mail:wangshangfree@gmail.com
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Old   April 13, 2019, 07:27
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Raśl Felipe Corrales Flores
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Hello dear Ralph

could I get the experimental data of naca0012?

my mail:rcorralesflores@gmail.com
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Old   January 9, 2020, 06:36
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Hi Ralph,

Could you share that information with me?

My e-mail is bakunnej@gmail.com

Thank you.
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Old   May 1, 2020, 20:50
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hi ralph

could I get the experimental data of NACA 0012 ?

this is my mail adress : burak.mavuk@pru.edu.tr

thanks
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Old   February 20, 2023, 04:08
Default Require Low reynolds number experimental data of naca 0012
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Can anyone share experimental results of naca 0012 of reynolds number order 10^5.
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Old   February 22, 2023, 10:03
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have you tried looking for NACA reports on the NASA technical reports server or looking through the data included in the freely available book Theory of Wing Sections?

But be warned... data for the NACA 0012 is not always self-consistent.
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