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Large-scale Advanced Prop-fan (LAP) technology assessment reportThe technologically significant findings and accomplishments of the Large Scale Advanced Prop-Fan (LAP) program in the areas of aerodynamics, aeroelasticity, acoustics and materials and fabrication are described. The extent to which the program goals related to these disciplines were achieved is discussed, and recommendations for additional research are presented. The LAP program consisted of the design, manufacture and testing of a near full-scale Prop-Fan or advanced turboprop capable of operating efficiently at speeds to Mach .8. An aeroelastically scaled model of the LAP was also designed and fabricated. The goal of the program was to acquire data on Prop-Fan performance that would indicate the technology readiness of Prop-Fans for practical applications in commercial and military aviation.
Document ID
19900000730
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Degeorge, C. L.
(Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
HSER-11804
NAS 1.26:182142
NASA-CR-182142
Report Number: HSER-11804
Report Number: NAS 1.26:182142
Report Number: NASA-CR-182142
Accession Number
90N10046
Funding Number(s)
CONTRACT_GRANT: NAS3-23051
PROJECT: RTOP 535-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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