Effects Of Independent Variation Of Mach And Reynolds Numbers On The Low Speed Aerodynamic Characteristics Of The Naca 0012 Airfoil Section
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Effects of Independent Variation of Mach and Reynolds Numbers on the Low-Speed Aerodynamic Characteristics of the NACA 0012 Airfoil Section
Author | : National Aeronautics and Space Adm Nasa |
Publisher | : |
Total Pages | : 98 |
Release | : 2018-11-07 |
Genre | : |
ISBN | : 9781730943355 |
Download Effects of Independent Variation of Mach and Reynolds Numbers on the Low-Speed Aerodynamic Characteristics of the NACA 0012 Airfoil Section Book in PDF, Epub and Kindle
A comprehensive data base is given for the low speed aerodynamic characteristics of the NACA 0012 airfoil section. The Langley low-turbulence pressure tunnel is the facility used to obtain the data. Included in the report are the effects of Mach number and Reynolds number and transition fixing on the aerodynamic characteristics. Presented are also comparisons of some of the results with previously published data and with theoretical estimates. The Mach number varied from 0.05 to 0.36. The Reynolds number, based on model chord, varied from 3 x 10 to the 6th to 12 x 10 to the 6th power. Ladson, Charles L. Langley Research Center...
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