An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift

Author: Maki, Ralph L
Year: 1956
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3871
Link: https://digital.library.unt.edu/ark:/67531/metadc56231/

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