Transonic aerodynamic characteristics of an NACA 64A006 airfoil section with a 15-percent-chord leading-edge flap.

Author: Humphreys, Milton D.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53G23
Link: https://digital.library.unt.edu/ark:/67531/metadc59751/

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