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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