Effects of spanwise thickness variation on the transonic aerodynamic characteristics of wings having 35 degrees of sweepback, aspect ratio 4, and taper ratio 0.60

Author: Morrison, William D., Jr.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51F28
Link: https://digital.library.unt.edu/ark:/67531/metadc58932/

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