Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections Page: 1 of 33
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NATIONAL ADVISORY COMMITTEE
z FOR AERONAUTICS
TECHNICAL NOTE 2824
EFFECTS OF INDEPENDENT VARIATIONS OF MACH NUMBER AND
REYNOLDS NUMBER ON THE MAXIMUM LIFT COEFFICIENTS
OF FOUR NACA 6-SERIES AIRFOIL SECTIONS
t By Stanley F. Racisz
Langley Aeronautical Laboratory
Langley Field, Va.
I i TE*P I I. sAlr Ir
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Racisz, Stanley F. Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections, report, November 1952; (digital.library.unt.edu/ark:/67531/metadc56326/m1/1/: accessed November 16, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.