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Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, 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-L9H22
Link:
https://digital.library.unt.edu/ark:/67531/metadc58309/
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