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Aircraft Engine Technology for Green Aviation to Reduce Fuel BurnThe NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Integrated Systems Research Program Environmentally Responsible Aviation Project in the Aeronautics Research Mission Directorate are conducting research on advanced aircraft technology to address the environmental goals of reducing fuel burn, noise and NOx emissions for aircraft in 2020 and beyond. Both Projects, in collaborative partnerships with U.S. Industry, Academia, and other Government Agencies, have made significant progress toward reaching the N+2 (2020) and N+3 (beyond 2025) installed fuel burn goals by fundamental aircraft engine technology development, subscale component experimental investigations, full scale integrated systems validation testing, and development validation of state of the art computation design and analysis codes. Specific areas of propulsion technology research are discussed and progress to date.
Document ID
20140003870
Document Type
Technical Memorandum (TM)
Authors
Hughes, Christopher E.
(NASA Glenn Research Center Cleveland, OH, United States)
VanZante, Dale E.
(NASA Glenn Research Center Cleveland, OH, United States)
Heidmann, James D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
April 28, 2014
Publication Date
November 1, 2013
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18373
NASA/TM-2013-217690
AIAA Paper 2011-3531
Meeting Information
Meeting: Atmospheric and Space Environments Conference
Location: Honolulu, HI
Country: United States
Start Date: June 27, 2011
End Date: June 30, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 699959.02.09.03.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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