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Aerodynamic Characteristics of an Airfoil-Forebody Swept Flying-Boat Hull With a Wing and Tail Swept Back 51.3 Degrees at the Leading Edge
Author:
Naeseth, Rodger L.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9F08
Link:
https://digital.library.unt.edu/ark:/67531/metadc58380/
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