An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 1: Characteristics of a Wing Having a Double-Wedge Airfoil Section With Maximum Thickness at 20-Percent Chord

Author: Anderson, Adrien E.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A7F06
Link: https://digital.library.unt.edu/ark:/67531/metadc64619/

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