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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