Low-Speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-Arc Airfoil Sections at Reynolds Numbers of Approximately 6.0 X 10(Exp 6)

Author: Spooner, Stanley H.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9A07
Link: https://digital.library.unt.edu/ark:/67531/metadc58210/

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