Wind-Tunnel Investigation of the Use of Leading-Edge and Trailing-Edge Area-Suction Flaps on a 13-Percent-Thick Straight Wing and Fuselage Model

Author: Holzhauser, Curt A.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A57K01
Link: https://digital.library.unt.edu/ark:/67531/metadc63996/

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