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Lift and drag values of NACA0015

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Old   February 8, 2001, 04:15
Default Lift and drag values of NACA0015
  #1
Marat Hoshim
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Hello,

I'm looking for 2D lift, drag and moment coefficients of a NACA0015 airfoil. Especially in the near stall range (aoa between 14 and 20 degrees)

Does someone know these values ?

Thanks,

Marat
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Old   February 8, 2001, 06:24
Default Re: Lift and drag values of NACA0015
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James Date
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These two Refs both have the 2D data on NACA 0015 you are looking for.

Shiba, H., "Model Experiments about the Maneuverability of Turning Ships," First Symposium on Ship Maneuvarability, DTRC Report 1461, October 1960.

Thieme, H., "Design of Ship Rudders," DTRC Translation No. 321, by E. N. LaBouvie, November 1965.

Regards

James
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Old   February 9, 2001, 02:48
Default Re: Lift and drag values of NACA0015
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Markus Lummer
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Hi Marat,

have a look at the original NACA report 586 from

http://naca.larc.nasa.gov/reports/1937/naca-report-586

Hope it helps!

Markus
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