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Aerodynamic Characteristics of a Wing With Quarter-Chord Line Swept Back 45 Degrees, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
Author:
Goodson, Kenneth W.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9I08
Link:
https://digital.library.unt.edu/ark:/67531/metadc58328/
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