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Prop-fan data support studyUpdated parametric prop-fan data packages are presented and the rationale used in developing the new prop-fan data is detailed. These data represent Hamilton Standard's projections of prop-fan characteristics for aircraft that are expected to be in-service in the 1985 to 1990 time frame. The basic prop-fan configuration was designed for efficient cruise operation at 0.8 Mach number and 10,668M altitude. The design blade tip speed is 244 mps and the design power loading is 301 KW/M squared.
Document ID
19780019185
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baum, J. A. (Hamilton Standard Windsor Locks, CT, United States)
Dumais, P. J. (Hamilton Standard Windsor Locks, CT, United States)
Mayo, M. G. (Hamilton Standard Windsor Locks, CT, United States)
Metzger, F. B. (Hamilton Standard Windsor Locks, CT, United States)
Shenkman, A. M. (Hamilton Standard Windsor Locks, CT, United States)
Walker, G. G. (Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
September 3, 2013
Publication Date
February 28, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-152141
Report Number: NASA-CR-152141
Accession Number
78N27128
Funding Number(s)
CONTRACT_GRANT: NAS2-9750
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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