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Accession Number:
ADB183080
Title:
The Effect of Blade-Section Thickness Ratios on the Aerodynamic Characteristics of Related Full-Scale Propellers at Mach Numbers up to 0.65
Descriptive Note:
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1953-01-01
Pagination or Media Count:
60.0
Abstract:
Distribution Statement:
APPROVED FOR PUBLIC RELEASE