The effects of trailing-edge flaps on the subsonic aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3

Author: Tinling, Bruce E.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A54L07
Link: https://digital.library.unt.edu/ark:/67531/metadc62223/

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