Aerodynamic characteristics at high and low subsonic Mach numbers of four NACA 6-series airfoil sections at angles of attack from -2 to 31 degrees

Author: Wilson, Homer B., Jr.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53C20
Link: https://digital.library.unt.edu/ark:/67531/metadc59710/

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