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The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section
Author:
Summers, James L.
Year:
1950
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2096
Link:
https://digital.library.unt.edu/ark:/67531/metadc55549/
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