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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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