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Advanced turboprop potential for high speedA turboprop propulsion system for general aviation aircraft, allowing high speed flight (to 0.8 Mach) is discussed. Design methodologies for aerodynamic and acoustic considerations and the performance and cost advantages of a prop-fan aircraft are presented.
Document ID
19800013856
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gatzen, B. S. (Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800013840Collected WorksGeneral Aviation Propulsion
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