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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