Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

Author: Abbott, Frank T , Jr
Year: 1942
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-701, NACA-MR
Link: https://digital.library.unt.edu/ark:/67531/metadc61351/

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