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August 4, 2009, 00:13 |
NACA 0012 data
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#1 |
New Member
Jules
Join Date: Jul 2009
Location: Sydney, Australia
Posts: 9
Rep Power: 16 |
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. |
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