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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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