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N+3 Aircraft Concept Designs and Trade StudiesMIT, Aerodyne Research, Aurora Flight Sciences, and Pratt & Whitney have collaborated to address NASA s desire to pursue revolutionary conceptual designs for a subsonic commercial transport that could enter service in the 2035 timeframe. The MIT team brings together multidisciplinary expertise and cutting-edge technologies to determine, in a rigorous and objective manner, the potential for improvements in noise, emissions, and performance for subsonic fixed wing transport aircraft. The collaboration incorporates assessment of the trade space in aerodynamics, propulsion, operations, and structures to ensure that the full spectrum of improvements is identified. Although the analysis focuses on these key areas, the team has taken a system-level approach to find the integrated solutions that offer the best balance in performance enhancements. Based on the trade space analyses and system-level assessment, two aircraft have been identified and carried through conceptual design to show both the in-depth engineering that underpins the benefits envisioned and also the technology paths that need to be followed to enable, within the next 25 years, the development of aircraft three generations ahead in capabilities from those flying today.
Document ID
20100042401
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Greitzer, E. M.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Bonnefoy, P. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
DelaRosaBlanco, E.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Dorbian, C. S.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Drela, M.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Hall, D. K.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Hansman, R. J.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Hileman, J. I.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Liebeck, R. H.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Levegren, J.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Mody, P.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Pertuze, J. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Sato, S.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Spakovszky, Z. S.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Tan, C. S.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Hollman, J. S.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Duda, J. E.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Fitzgerald, N.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Houghton, J.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Kerrebrock, J. L.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Kiwada, G. F.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Kordonowy, D.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Parrish, J. C.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Tylko, J.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Wen, E. A.
(Aurora Flight Sciences, Inc. Cambridge, MA, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
E-17419-1
NASA/CR-2010-216794/VOL1
Funding Number(s)
WBS: WBS 561581.02.08.03.13.03
CONTRACT_GRANT: NNX08AW63A
Distribution Limits
Public
Copyright
Public Use Permitted.
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