An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 2: The Effect of Airfoil Section Modifications and the Determination of the Wake Downwash

Author: Anderson, Adrien E.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A7H28
Link: https://digital.library.unt.edu/ark:/67531/metadc58089/

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