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prasad84 July 8, 2011 12:50

NACA 0012 Experimental Data
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?


f-w July 11, 2011 12:34

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:

syler3321 July 15, 2011 01:09

Give me your email addy and i'll send the experimental data to you.


prasad84 July 20, 2011 12:45

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.

veda February 22, 2016 03:24

Experimental data for NACA 0012 please can you send the experimental data file to the above mail.

G S Srivatsa June 18, 2016 02:05

Help Needed
I'm doing a project on NACA 0012 please send me the experimental data of the air foil
my email id is

sajad6 December 4, 2016 01:41

validation of incompressible laminar flow solver
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?

Hulk_25 April 6, 2017 06:23

Experimental data for Naca 0012
Hey guys,

I have gone onto the website and I have looked everywhere. What I need is the lift and drag coefficient of the experimental data for this airfoil, can anyone help?

fluid23 April 6, 2017 14:53

Good luck. There are several conflicting data sets available for this airfoil. You are better off choosing a different profile for validation.

mnazar May 28, 2017 10:15
please also send me it

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