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Advanced technology transport configuration.Consideration of the compromises involved in advanced transport aircraft designs for Mach numbers approaching 1.0, to develop an environmentally acceptable and economically viable commercial transport. The impact of configuration constraints on a baseline aircraft is discussed, and details are given on the development of the aircraft from a wind tunnel model. The subjects covered also include the configuration cycle, aerodynamic and configuration concepts, full-scale aircraft characteristics, and an alternate aircraft configuration.
Document ID
19720056390
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, B. (Boeing Co., Commercial Airplane Group, Seattle Wash., United States)
Date Acquired
August 6, 2013
Publication Date
August 1, 1972
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 72-756
Report Number: AIAA PAPER 72-756
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aircraft Design, Flight Test, and Operations Meeting
Location: Los Angeles, CA
Start Date: August 7, 1972
End Date: August 9, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A40056
Funding Number(s)
CONTRACT_GRANT: NAS1-10703
Distribution Limits
Public
Copyright
Other

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