CFD Online Discussion Forums

CFD Online Discussion Forums (http://www.cfd-online.com/Forums/)
-   Main CFD Forum (http://www.cfd-online.com/Forums/main/)
-   -   Search for cd and cl experimental results of NACA 0012 (http://www.cfd-online.com/Forums/main/99911-search-cd-cl-experimental-results-naca-0012-a.html)

spk April 15, 2012 15:22

Search for cd and cl experimental results of NACA 0012
 
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!!

spk

agd April 15, 2012 19:00

Google

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

First result for a search on "lift coefficient NACA0012 3 million"

spk April 16, 2012 07:49

Thanks a lot! :)
I search for accurate experimental data of cl and cd, like a table with the values of cl and cd!

spk April 17, 2012 14:28

Quote:

Originally Posted by agd (Post 354804)
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


All times are GMT -4. The time now is 14:20.