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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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