Pressure-distribution data for the NACA 64(sub 1)-012 and 64(sub 1) A012 airfoils at high subsonic Mach numbers

Author: Humphreys, Milton D
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9C18
Link: https://digital.library.unt.edu/ark:/67531/metadc58257/

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