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NASA Collaborative Research on the Ultra High Bypass Engine Cycle and Potential Benefits for Noise, Performance, and EmissionsThe National Aeronautics and Space Administration has taken an active role in collaborative research with the U.S. aerospace industry to investigate technologies to minimize the impact of aviation on the environment. In December 2006, a new program, called the Fundamental Aeronautics Program, was established to enhance U.S. aeronautics technology and conduct research on energy, efficiency and the environment. A project within the overall program, the Subsonic Fixed Wing Project, was formed to focus on research related to subsonic aircraft with specific goals and time based milestones to reduce aircraft noise, emissions and fuel burn. This paper will present an overview of the Subsonic Fixed Wing Project environmental goals and describe a segment of the current research within NASA and also were worked collaboratively with partners from the U.S. aerospace industry related to the next generation of aircraft that will have lower noise, emissions and fuel burn.
Document ID
20140004373
Document Type
Technical Memorandum (TM)
Authors
Hughes, Christopher E. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
May 1, 2014
Publication Date
November 1, 2013
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
E-17282
ISABE-2009-1274
NASA/TM-2013-216345
Meeting Information
International Symposium on Air Breathing Engines (ISABE 2009)(Montreal, Quebec)
Funding Number(s)
WBS: WBS 561581.02.08.03.11.55
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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