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AVION: A detailed report on the preliminary design of a 79-passenger, high-efficiency, commercial transport aircraftThe Avion is the result of an investigation into the preliminary design for a high-efficiency commercial transport aircraft. The Avion is designed to carry 79 passengers and a crew of five through a range of 1,500 nm at 455 kts (M=0.78 at 32,000 ft). It has a gross take-off weight of 77,000 lb and an empty weight of 42,400 lb. Currently there are no American-built aircraft designed to fit the 60 to 90 passenger, short/medium range marketplace. The Avion gathers the premier engineering achievements of flight technology and integrates them into an aircraft which will challenge the current standards of flight efficiency, reliability, and performance. The Avion will increase flight efficiency through reduction of structural weight and the improvement of aerodynamic characteristics and propulsion systems. Its design departs from conventional aircraft design tradition with the incorporation of a three-lifting-surface (or tri-wing) configuration. Further aerodynamic improvements are obtained through modest main wing forward sweeping, variable incidence canards, aerodynamic coupling between the canard and main wing, leading edge extensions, winglets, an aerodynamic tailcone, and a T-tail empennage. The Avion is propelled by propfans, which are one of the most promising developments for raising propulsive efficiencies at high subsonic Mach numbers. Special attention is placed on overall configuration, fuselage layout, performance estimations, component weight estimations, and planform design. Leading U.S. technology promises highly efficient flight for the 21st century; the Avion will fulfill this promise to passenger transport aviation.
Document ID
19900014079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mayfield, William
(Auburn Univ. AL, United States)
Perkins, Brett
(Auburn Univ. AL, United States)
Rogan, William
(Auburn Univ. AL, United States)
Schuessler, Randall
(Auburn Univ. AL, United States)
Stockert, Joe
(Auburn Univ. AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-186663
NAS 1.26:186663
Report Number: NASA-CR-186663
Report Number: NAS 1.26:186663
Accession Number
90N23395
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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