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Tests of Four Full-scale Propellers to Determine the Effect of Trailing-edge Extensions on Propeller Aerodynamic CharacteristicsPropellers with trailing-edge extensions were studied to determine aerodynamic characteristics. Trailing-edge extension increased power absorbed by propeller with little loss in efficiency. Power coefficient for maximum efficiency was greater for 20% camber type extension than for 20% straight type extension over range of advance ratio of 1.0 to 2.5 although camber type was less efficient. Efficiency was about the same for cruising and high-speed at a high power coefficient for propeller with extension.
Document ID
19930093330
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Maynard, Julian D.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Evans, Albert J
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1945
Subject Category
Aerodynamics
Report/Patent Number
NACA-WR-L-582
Report Number: NACA-WR-L-582
Accession Number
93R22620
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPELLERS - TRAILING EDGE, EXTENDED
PROPELLERS - CHARACTERISTICS WIND TUNNEL TESTS (NACA -
PROPELLERS - CURTISS WIND TUNNEL TESTS (NACA -
WIND TUNNEL TESTS - NACA - HIGH-SPEED (16FT)
CHARTS - PROPELLERS
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