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Looking for 3D wind tunnel airfoil(wing) experimental data for CFD validation

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Old   June 4, 2015, 09:41
Default Looking for 3D wind tunnel airfoil(wing) experimental data for CFD validation
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Hi all,

Currently I need to model the 3D wing for lift and drag coefficient calculations. I need some 3D wind tunnel experimental data for the CFD validation so that I can feel more comfortable about my simulation data. Where could I find these 3D experimental data?

thanks!!!
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Old   June 4, 2015, 12:53
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Try googling "ONERA M6"
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Old   June 4, 2015, 14:26
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As agd suggests, ONERA M6 is a good option. Here are some others that I have used in the past as well...

Weber, J. and Brebner, G.G., ‘Low Speed Tests on 45-deg Swept-Back Wings. Part 1: Pressure Measurements on Wings of Aspect Ratio 5,’ Aeronautical Research Council, RM-2882, London, England, UK, 1958.

Hall, I.M. and Rogers, E.W.E, ‘Experiments with a Tapered Sweptback Wing of Warren 12 Planform at Mach Numbers between 0.6 and 1.6,’ Aeronautical Research Council, RM-3271, London, England, UK, 1962



Kolbe. C.D. and Boltz, F.W., ‘The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45
Sweepback, Aspect Ratio of 3, and a Taper Ratio of 0.5,’ NACA RM-451G31, National Advisory Committee for Aeronautics, 1951.



Graham, R.R., ‘Low-Speed Characteristics of a 45 Sweptback Wing of Aspect Ratio 8 from Pressure Distribution and Force Tests at Reynolds Numbers from 1,500,000 to 4,800,000,’NACA RM-L51H13, National Advisory Committee for Aeronautics, 1951.



McAlister, K.W. and Takahasi, R.K., ‘NACA 0015 Wing Pressure and Trailing Vortex
Mesurements,’ NASA TP 3151, National Aeronautics and Space Administration,. Washington, D.C., 1991.


Jacobs, W., ‘Pressure-Distribution Measurements on Unyawed Swept-Back Wings,’ NACA TM 1164, National Advisory Committee for Aeronautics, Washington, D.C., 1947.


Johnson, H.S. and Hagerman, J.R., ‘Wind-Tunnel Investigation at Low Speed of An Unswept Untapered Semispan Wing of Aspect Ratio 3.13 Equiped with Various 25-Percent-Chord Plain Flaps,’ NACA TN 2080, National Advisory Committee for Aeronautics, Washington, D.C., 1950.


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Old   June 4, 2015, 22:01
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Quote:
Originally Posted by agd View Post
Try googling "ONERA M6"
thank u very much!
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Old   June 4, 2015, 22:04
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Quote:
Originally Posted by MBdonCFD View Post
As agd suggests, ONERA M6 is a good option. Here are some others that I have used in the past as well...

Weber, J. and Brebner, G.G., ‘Low Speed Tests on 45-deg Swept-Back Wings. Part 1: Pressure Measurements on Wings of Aspect Ratio 5,’ Aeronautical Research Council, RM-2882, London, England, UK, 1958.

Hall, I.M. and Rogers, E.W.E, ‘Experiments with a Tapered Sweptback Wing of Warren 12 Planform at Mach Numbers between 0.6 and 1.6,’ Aeronautical Research Council, RM-3271, London, England, UK, 1962



Kolbe. C.D. and Boltz, F.W., ‘The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45
Sweepback, Aspect Ratio of 3, and a Taper Ratio of 0.5,’ NACA RM-451G31, National Advisory Committee for Aeronautics, 1951.



Graham, R.R., ‘Low-Speed Characteristics of a 45 Sweptback Wing of Aspect Ratio 8 from Pressure Distribution and Force Tests at Reynolds Numbers from 1,500,000 to 4,800,000,’NACA RM-L51H13, National Advisory Committee for Aeronautics, 1951.



McAlister, K.W. and Takahasi, R.K., ‘NACA 0015 Wing Pressure and Trailing Vortex
Mesurements,’ NASA TP 3151, National Aeronautics and Space Administration,. Washington, D.C., 1991.


Jacobs, W., ‘Pressure-Distribution Measurements on Unyawed Swept-Back Wings,’ NACA TM 1164, National Advisory Committee for Aeronautics, Washington, D.C., 1947.


Johnson, H.S. and Hagerman, J.R., ‘Wind-Tunnel Investigation at Low Speed of An Unswept Untapered Semispan Wing of Aspect Ratio 3.13 Equiped with Various 25-Percent-Chord Plain Flaps,’ NACA TN 2080, National Advisory Committee for Aeronautics, Washington, D.C., 1950.


Thank you very much for your answer. It's very helpful!
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