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The outlook for advanced transport aircraftThe technological advances most likely to contribute to advanced aircraft designs and the efficiency, performance, and financial considerations driving the development directions for new aircraft are reviewed. Fuel-efficiency is perceived as the most critical factor for any new aircraft or component design, with most gains expected to come in areas of propulsion, aerodynamics, configurations, structural designs and materials, active controls, digital avionics, laminar flow control, and air-traffic control improvements. Any component area offers an efficiency improvement of 3-12%, with a maximum of 50% possible with a 4000 m range aircraft. Advanced turboprops have potential applications in short and medium haul subsonic aircraft, while a fuel efficient SST may be possible by the year 2000. Further discussion is devoted to the pivoted oblique wing aircraft, lightweight structures, and the necessity for short payback times.
Document ID
19820037839
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Leavens, J. M., Jr.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Schaufele, R. D.
(Douglas Aircraft Co. Long Beach, CA, United States)
Jones, R. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Steiner, J. E.
(Boeing Co. Seattle, WA, United States)
Beteille, R.
(AirBus Industrie Blagnac, Haute-Garonne, France)
Titcomb, G. A.
(United Technologies Corp. Pratt and Whitney Aircraft Group, East Hartford, CT, United States)
Coplin, J. F.
(Rolls-Royce, Ltd. London, United Kingdom)
Rowe, B. H.
(General Electric Co., Aircraft Engine Group, Cincinnati OH, United States)
Lloyd-Jones, D. J.
(American Airlines, Inc. Fort Worth, TX, United States)
Overend, W. J.
(Delta Air Lines, Inc. Atlanta, GA, United States)
Date Acquired
August 10, 2013
Publication Date
February 1, 1982
Publication Information
Publication: Astronautics and Aeronautics
Volume: 20
Subject Category
Aircraft Design, Testing And Performance
Accession Number
82A21374
Distribution Limits
Public
Copyright
Other

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