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Small-scale transonic investigation of the effects of twist and camber on the aerodynamic characteristics of a 60 degrees 42' sweptback wing of aspect ratio 1.94
Author:
Spreemann, Kenneth P.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51I21
Link:
https://digital.library.unt.edu/ark:/67531/metadc59044/
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