NDLI: Fuel savings potential of the nasa advanced turboprop program

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Fuel savings potential of the nasa advanced turboprop program

Content Provider	NASA Technical Reports Server (NTRS)
Author	Sievers, G. K. Whitlow Jr., J. B.
Copyright Year	1984
Description	The NASA Advanced Turboprop (ATP) Program is directed at developing new technology for highly loaded, multibladed propellers for use at Mach 0.65 to 0.85 and at altitudes compatible with the air transport system requirements. Advanced turboprop engines offer the potential of 15 to 30 percent savings in aircraft block fuel relative to advanced turbofan engines (50 to 60 percent savings over today's turbofan fleet). The concept, propulsive efficiency gains, block fuel savings and other benefits, and the program objectives through a systems approach are described. Current program status and major accomplishments in both single rotation and counter rotation propeller technology are addressed. The overall program from scale model wind tunnel tests to large scale flight tests on testbed aircraft is discussed.
File Size	9916891
Page Count	62
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840021809
Archival Resource Key	ark:/13960/t9n34pr4s
Language	English
Publisher Date	1984-01-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Flight Tests Energy Conservation Efficiency Wind Tunnel Tests Fuel Consumption Commercial Aircraft Propeller Efficiency Turboprop Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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