Aerodynamic Tests of an NACA 66(215)-116, a=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane

Author: Cahill, Jones F.
Year: 1944
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-629, NACA-MR-L4K21
Link: https://digital.library.unt.edu/ark:/67531/metadc61411/

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