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Advanced subsonic transport propulsionA brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in this review are the factors that influenced the design of these turbofan engines and the advanced technology incorporated in them to reduce fuel consumption and improve environmental characteristics. In addition, factors such as the continuing spiral in fuel cost, that could influence future aircraft propulsion systems beyond those represented by the E(3) engines, are also discussed. Advanced technologies that will address these influencing factors and provide viable future propulsion systems are described. The potential importance of other propulsion system types, such as geared fans and turboshaft engines, is presented.
Document ID
19810022653
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nored, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Ciepluch, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamberlain, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Meleason, E. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Kraft, G. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-979
NASA-TM-82696
Report Number: E-979
Report Number: NASA-TM-82696
Accession Number
81N31195
Funding Number(s)
PROJECT: RTOP 535-01-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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