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NASA advanced turboprop research and concept validation programNASA has determined by experimental and analytical effort that use of advanced turboprop propulsion instead of the conventional turbofans in the older narrow-body airline fleet could reduce fuel consumption for this type of aircraft by up to 50 percent. In cooperation with industry, NASA has defined and implemented an Advanced Turboprop (ATP) program to develop and validate the technology required for these new high-speed, multibladed, thin, swept propeller concepts. This paper presents an overview of the analysis, model-scale test, and large-scale flight test elements of the program together with preliminary test results, as available.
Document ID
19880013518
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitlow, John B., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Sievers, G. Keith
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-4129
NAS 1.15:100891
NASA-TM-100891
Accession Number
88N22902
Funding Number(s)
PROJECT: RTOP 535-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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