Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps

Author: Fullmer, Felicien F., Jr.
Year: 1944
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-140, NACA-CB-L4G10
Link: https://digital.library.unt.edu/ark:/67531/metadc61376/

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