Lift Tests of a 0.1536c Thick Douglas Airfoil Section of NACA 7-Series Type Equipped With a Lateral-Control Device for Use With a Full-Span Double-Slotted Flap on the C-74 Airplane

Author: Nuber, Robert J.
Year: 1945
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-641, NACA-MR-L5C24a
Link: https://digital.library.unt.edu/ark:/67531/metadc61291/

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