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Environmentally Responsible Aviation (ERA) Project - N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV) Final ReportNASA has set demanding goals for technology developments to meet national needs to improve fuel efficiency concurrent with improving the environment to enable air transportation growth. A figure shows NASA's subsonic transport system metrics. The results of Boeing ERA N+2 Advanced Vehicle Concept Study show that the Blended Wing Body (BWB) vehicle, with ultra high bypass propulsion systems have the potential to meet the combined NASA ERA N+2 goals. This study had 3 main activities. 1) The development of an advanced vehicle concepts that can meet the NASA system level metrics. 2) Identification of key enabling technologies and the development of technology roadmaps and maturation plans. 3) The development of a subscale test vehicle that can demonstrate and mature the key enabling technologies needed to meet the NASA system level metrics. Technology maturation plans are presented and include key performance parameters and technical performance measures. The plans describe the risks that will be reduced with technology development and the expected progression of technical maturity.
Document ID
20140005559
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Bonet, John T.
(Boeing Research and Technology Huntington Beach, CA, United States)
Schellenger, Harvey G.
(Boeing Research and Technology Huntington Beach, CA, United States)
Rawdon, Blaine K.
(Boeing Research and Technology Huntington Beach, CA, United States)
Elmer, Kevin R.
(Boeing Research and Technology Huntington Beach, CA, United States)
Wakayama, Sean R.
(Boeing Research and Technology Huntington Beach, CA, United States)
Brown, Derrell L.
(Boeing Research and Technology Huntington Beach, CA, United States)
Guo, Yueping
(Boeing Research and Technology Huntington Beach, CA, United States)
Date Acquired
May 12, 2014
Publication Date
December 1, 2011
Subject Category
Aircraft Design, Testing And Performance
Air Transportation And Safety
Report/Patent Number
DFRC-E-DAA-TN8572
NASA/CR-2011-216519
Funding Number(s)
CONTRACT_GRANT: NND11AG03C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aircraft Engines
Laminar Flow
Turbofans
Acoustics
Aircraft Design
Composite Materials
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