Search for cd and cl experimental results of NACA 0012

spk · April 15, 2012, 16:22

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, 20:00

Google

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

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

spk · April 16, 2012, 08:49

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, 15:28

Quote:

Originally Posted by agd

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

April 15, 2012, 16:22	Search for cd and cl experimental results of NACA 0012	#1
spk Member Join Date: Aug 2009 Posts: 67 Rep Power: 17	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

April 15, 2012, 20:00		#2
agd Senior Member Join Date: Jul 2009 Posts: 358 Rep Power: 19	Google http://turbmodels.larc.nasa.gov/naca0012_val.html First result for a search on "lift coefficient NACA0012 3 million"

April 16, 2012, 08:49		#3
spk Member Join Date: Aug 2009 Posts: 67 Rep Power: 17	Thanks a lot! I search for accurate experimental data of cl and cd, like a table with the values of cl and cd!