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Evaluation of a Hydrogen Fuel Cell Powered Blended-Wing-Body Aircraft Concept 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 blended-wing-body configuration with advanced technology hydrogen fuel cell electric propulsion is considered. Predicted noise and emission characteristics are compared to a current technology conventional configuration designed for the same mission. The significant technology issues which have to be addressed to make this 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 was initiated to develop revolutionary concepts that address strategic objectives of the NASA Enterprises, such as reducing aircraft noise and emissions, and to identify advanced technology requirements for the concepts.
Document ID
20040033924
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Guynn, Mark D.
(NASA Langley Research Center Hampton, VA, United States)
Freh, Joshua E.
(NASA Glenn Research Center Cleveland, OH, United States)
Olson, Erik D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-18342
NASA/TM-2004-212989
Funding Number(s)
WORK_UNIT: WU 23-755-81-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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