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High-speed-propeller wind-tunnel aeroacoustic resultsSome aerodynamic concepts are presented together with an explanation of how these concepts are applied to advanced propeller design. The unique features of this propulsion system are addressed with emphasis on the design concepts being considered for the high speed turboprop. More particular emphasis is given to the blade sweep, long blade chords, and the large number of blades.
Document ID
19800013857
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jeracki, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Dittmar, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22344
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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