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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