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Off-design analysis of counter-rotating propeller configurationsAn analysis is conducted to determine whether the counterrotating propeller configuration maintains, and perhaps improves, its excellent performance in the off-design mode for the constant-speed or variable-pitch case. While the twist distribution is maintained, the blade angle is changed to absorb shaft horsepower as a constant rpm setting is maintained under varying freestream velocities. A relatively flat propeller efficiency curve is obtained for advance ratios of 1.5-5.0.
Document ID
19870040715
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Korkan, K. D.
(Texas A&M Univ. College Station, TX, United States)
Gazzaniga, J. A.
(Texas A & M University College Station, United States)
Date Acquired
August 13, 2013
Publication Date
February 1, 1987
Publication Information
Publication: Journal of Propulsion and Power
Volume: 3
ISSN: 0748-4658
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ISSN: 0748-4658
Accession Number
87A27989
Funding Number(s)
CONTRACT_GRANT: NAG3-354
Distribution Limits
Public
Copyright
Other

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