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#1 |
New Member
Prasad
Join Date: Jul 2009
Posts: 6
Rep Power: 15 ![]() |
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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#2 |
Senior Member
Join Date: Apr 2009
Posts: 144
Rep Power: 15 ![]() |
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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#3 |
Member
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Give me your email addy and i'll send the experimental data to you.
Ralph |
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#4 |
New Member
Prasad
Join Date: Jul 2009
Posts: 6
Rep Power: 15 ![]() |
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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#5 |
New Member
VEDA MURTHY VEDANTHAM
Join Date: Dec 2014
Posts: 2
Rep Power: 0 ![]() |
vedavvdvvm@gmail.com please can you send the experimental data file to the above mail.
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#6 |
New Member
Grama Srivatsa
Join Date: Jun 2016
Posts: 2
Rep Power: 0 ![]() |
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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#7 |
Member
sajad
Join Date: Apr 2014
Location: Iran
Posts: 46
Rep Power: 10 ![]() |
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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#8 |
New Member
Reuben
Join Date: Apr 2017
Posts: 1
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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 06:24. Reason: Clarity |
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#9 |
Senior Member
Matt
Join Date: Aug 2014
Posts: 931
Rep Power: 16 ![]() |
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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#10 |
Member
hgggfh
Join Date: Jan 2017
Posts: 30
Rep Power: 8 ![]() |
mhammadjawad95@gmail.com
please also send me it |
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#11 |
New Member
Katharina
Join Date: Jan 2018
Posts: 1
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#12 |
New Member
Ebubekir
Join Date: Nov 2017
Posts: 4
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#13 |
New Member
Join Date: May 2018
Posts: 1
Rep Power: 0 ![]() |
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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#14 |
New Member
Kamyar
Join Date: Dec 2018
Posts: 2
Rep Power: 0 ![]() |
Hello dear Ralph
could you please send me the experimental data of naca0012? my mail:k.nav1996@gmail.com |
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#15 |
New Member
Join Date: Aug 2017
Posts: 9
Rep Power: 7 ![]() |
Hello dear Ralph
could I get the experimental data of naca0012? my mail:wangshangfree@gmail.com |
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#16 |
New Member
Raśl Felipe Corrales Flores
Join Date: Dec 2017
Posts: 1
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Hello dear Ralph
could I get the experimental data of naca0012? my mail:rcorralesflores@gmail.com |
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#17 |
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Jose Manuel
Join Date: Jan 2020
Posts: 1
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#18 |
New Member
burak
Join Date: Feb 2020
Posts: 6
Rep Power: 5 ![]() |
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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#19 |
New Member
Javed
Join Date: Feb 2023
Posts: 1
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Can anyone share experimental results of naca 0012 of reynolds number order 10^5.
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#20 |
Senior Member
Matt
Join Date: Aug 2014
Posts: 931
Rep Power: 16 ![]() |
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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