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The Effect of Blade-Section Thickness Ratios on the Aerodynamic Characteristics of Related Full-Scale Propellers at Mach Numbers Up to 0.65
Author:
Maynard, Julian D.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9D29
Link:
https://digital.library.unt.edu/ark:/67531/metadc58288/
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