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Old   October 31, 2002, 17:21
Default NACA0012 exp.results
  #1
muygun
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Please help me, I need experimental pressure distibutions over NACA 0012-14-16 symmetric profiles at Re=5,6,9 millions. Thanks a lot.
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Old   November 1, 2002, 10:08
Default Re: NACA0012 exp.results
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Anders
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Hi, Did you search the NASA technical report service at:

http://naca.larc.nasa.gov/reports

A lot of pdf files may be downloaded from there.

Regards Anders
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Old   November 1, 2002, 12:33
Default Re: NACA0012 exp.results
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muygun
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Thanks Anders, I searched that web adress but I couldn't find exactly what I want especially pressure distrbutions for subsonic incompressible flows.
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Old   November 5, 2002, 01:01
Default Re: NACA0012 exp.results
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boling
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I guess you could find that in AGARD AR-138
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Old   November 9, 2002, 20:11
Default Re: NACA0012 exp.results
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ZIBI
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use XFOIL
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Old   November 11, 2002, 17:08
Default Re: NACA0012 exp.results
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James Date
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J.J Thibert, M. Grandjacques, and L.H. Oham, "NACA 0012 Airfoil", AGARD Advisory Report, 1979.

N. Gregory and O.L. O'Reilly, "Low Speed Aerodynamic Characteristics of NACA0012 Airfoil Section, Including the Effects of Upper Surface Roughness Simulation Hoarfrost", NPL Aero Report 1308, National Physical Laboratory 1970.

I think one of the these reports will have what you are looking for.

Reagrds

James Date
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Old   November 11, 2002, 18:40
Default Re: NACA0012 exp.results
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muygun
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Thanks a lot James.
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Old   November 11, 2002, 18:41
Default Re: NACA0012 exp.results
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muygun
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Thanks a lot, Boling
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