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Aerodynamic Characteristics of a 45 Degree Swept-Back Wing With Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
Author:
Proterra, Anthony J.
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L7C11
Link:
https://digital.library.unt.edu/ark:/67531/metadc58041/
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