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Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984In comparison to turbo-prop applications, the Prop-Fan is designed to operate in a significantly higher range of aircraft flight speeds. Two concerns arise regarding operation at very high speeds: aerodynamic performance and noise generation. This data package covers both topics over a broad range of operating conditions for the eight (8) bladed SR-7L Prop-Fan. Operating conditions covered are: Flight Mach Number 0 - 0.85; blade tip speed 600-800 ft/sec; and cruise power loading 20-40 SHP/D2. Prop-Fan weight and weight scaling estimates are also included.
Document ID
19850014057
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Parzych, D.
(Hamilton Standard Windsor Locks, CT, United States)
Shenkman, A.
(Hamilton Standard Windsor Locks, CT, United States)
Cohen, S.
(Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:174782
NASA-CR-174782
SP-06A83
Accession Number
85N22368
Funding Number(s)
PROJECT: RTOP 535-03-12
CONTRACT_GRANT: NAS3-23051
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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