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The Effect of Blade-Section Thickness Ratio on the Aerodynamic Characteristics of Related Full-Scale Propellers at Mach Numbers up to 0.65The results of an investigation of two 10-foot-diameter, two-blade NACA propellers are presented for a range of blade angles from 20 degrees to 55 degrees at airspeeds up to 500 miles per hour. These results are compared with those from previous investigations of five related NACA propellers in order to evaluate the effects of blade-section thickness ratios on propeller aerodynamic characteristics.
Document ID
19930092161
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Maynard, Julian D
Steinberg, Seymour
Date Acquired
September 6, 2013
Publication Date
January 1, 1953
Report/Patent Number
NACA-TR-1126
Report Number: NACA-TR-1126
Accession Number
93R21451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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