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effects of independent variation of mach and reynolds numbers on the low-speed aerodynamic characteristics of the naca 0012 airfoil sectionA 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.
Document ID
19880019495
Document Type
Technical Memorandum (TM)
Authors
Ladson, Charles L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Subject Category
AERONAUTICS (GENERAL)
Report/Patent Number
L-16472
NASA-TM-4074
NAS 1.15:4074
Funding Number(s)
PROJECT: RTOP 505-61-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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