Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section
Charles L. Ladson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988 - 94 pages
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0.05c location 0.15 for Transition 00 Alpha 0012 airfoil section 80 grit angle of attack attack for various basic aerodynamic characteristics carborundum characteristics with angle comparison data base drag coefficient EOOO Eppler code experimental lift-curve slopes Figure 17 fixed transition Force Coefficients free and fixed free transition frOOO ID a/i increasing Reynolds number Langley Low-Turbulence Pressure Langley Research Center little effect Low-Speed Aerodynamic Characteristics Low-Turbulence Pressure Tunnel Mach and Reynolds maximum lift coefficient maximum lift-drag ratio minimum drag NACA 0012 airfoil NASA number affect number and Reynolds number for free number for free-transition number range orifices percent previously published data stagnation pressure Stevens theory test program theoretical values TOO0 TOOO total-pressure tubes Transition Fixed transition location Tunnel center line turbulence level Variation of basic Variation of Mach Variation with Reynolds various Reynolds numbers wake survey rake Wind Tunnel xooo zero lift zooo