Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63(sub 1)-012 airfoil section

Author: Kelly, John A.
Year: 1950
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2228
Link: https://digital.library.unt.edu/ark:/67531/metadc55609/

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