CFD Online Discussion Forums

CFD Online Discussion Forums (http://www.cfd-online.com/Forums/)
-   Main CFD Forum (http://www.cfd-online.com/Forums/main/)
-   -   NACA 0012 data (http://www.cfd-online.com/Forums/main/67101-naca-0012-data.html)

pixie August 4, 2009 00:13

NACA 0012 data
 
Hi

I need some help please. I am looking at analyzing NACA 0012 airfoil using Fluent for a range of M (subsonic, transonic and supersonic) and angle of attacks. I am looking for reliable data – I have the book the theory of wing sections as well as a paper on experimental data ‘A Critical Assessment of Wind Tunnel Results for the NACA0012 Airfoil’ . However, in both these cases the results are very hard to read from the graphs and I'm worried about accuracy, so I would like to know if there is any way that I can get the data in tabular form or just better readable. Sorry if this is a stupid request, but I need something reliable to compare my data to.
Thank you.
:)

naveen August 4, 2009 04:52

0012 airfoil data
 
hi pixie

search this book in google, u wil find the results for naca 0012 airfoil case....

NPL 9615 and NACA 0012 :A Comparison of Aerodynamic Data BY "N. Gregory and P. G. Wilby Aerodynamics Division", NPL

Ahmed August 5, 2009 01:08

Quote:

Originally Posted by naveen (Post 225190)
hi pixie

search this book in google, u wil find the results for naca 0012 airfoil case....

NPL 9615 and NACA 0012 :A Comparison of Aerodynamic Data BY "N. Gregory and P. G. Wilby Aerodynamics Division", NPL

The following link might help, with the mesh included
http://www.aero.polimi.it/freecase/?...A_0012_airfoil

pixie August 5, 2009 03:01

thanx guys :)


All times are GMT -4. The time now is 04:40.