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Old   March 22, 2011, 09:59
Default NACA 0015 data
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Nicholas
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Hi,

I am currently running some simulations of a NACA 0015 which involve looking at the BL shape factor over the suction surface of the wing for various angles of incidence. My results are close to those given by a viscous analysis using XFoil.

Has anyone come across any experimental data of BL shape factor for a NACA 0015 at various incidence angles, so I can verify my results?

Thanks in advance,
Nick
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Old   March 23, 2011, 12:14
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Quote:
Originally Posted by en51nm View Post
Hi,

I am currently running some simulations of a NACA 0015 which involve looking at the BL shape factor over the suction surface of the wing for various angles of incidence. My results are close to those given by a viscous analysis using XFoil.

Has anyone come across any experimental data of BL shape factor for a NACA 0015 at various incidence angles, so I can verify my results?

Thanks in advance,
Nick
hi
may this help you

http://www.cyberiad.net/library/airf...ta/n0015cl.htm
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Old   March 23, 2011, 12:16
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Thanks for your reply, but unfortunately it's BL shape factor (or displacement and momentum thickness!) that I need.
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