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Evaluation of an Aircraft Concept With Over-Wing, Hydrogen-Fueled Engines for Reduced Noise and EmissionsThis report describes the analytical modeling and evaluation of an unconventional commercial transport aircraft concept designed to address aircraft noise and emission issues. A strut-braced wing configuration with overwing, ultra-high bypass ratio, hydrogen fueled turbofan engines is considered. Estimated noise and emission characteristics are compared to a conventional configuration designed for the same mission and significant benefits are identified. The design challenges and technology issues which would have to be addressed to make the concept a viable alternative to current aircraft designs are discussed. This concept is one of the "Quiet Green Transport" aircraft concepts studied as part of NASA's Revolutionary Aerospace Systems Concepts (RASC) Program. The RASC Program seeks to develop revolutionary concepts that address strategic objectives of the NASA Enterprises, such as reducing aircraft noise and emissions, and to identify enabling advanced technology requirements for the concepts.
Document ID
20020079419
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Guynn, Mark D.
(NASA Langley Research Center Hampton, VA United States)
Olson, Erik D.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2002
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-2002-211926
L-18222
NAS 1.15:211926
Report Number: NASA/TM-2002-211926
Report Number: L-18222
Report Number: NAS 1.15:211926
Funding Number(s)
PROJECT: RTOP 706-87-11-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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