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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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