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Advanced Configurations for Very Large Subsonic Transport AirplanesRecent aerospace industry interest in developing a subsonic commercial transport airplane with 50 percent greater passenger capacity than the largest existing aircraft in this category (the Boeing 747-400 with approximately 400-450 seats) has generated a range of proposals based largely on the configuration paradigm established nearly 50 years ago with the Boeing B-47 bomber. While this basic configuration paradigm has come to dominate subsonic commercial airplane development since the advent of the Boeing 707/Douglas DC-8 in the mid-1950's, its extrapolation to the size required to carry more than 600-700 passengers raises several questions. To explore these and a number of related issues, a team of Boeing, university, and NASA engineers was formed under the auspices of the NASA Advanced Concepts Program. The results of a Research Analysis focused on a large, unconventional transport airplane configuration for which Boeing has applied for a patent are the subject of this report. It should be noted here that this study has been conducted independently of the Boeing New Large Airplane (NLA) program, and with the exception of some generic analysis tools which may be common to this effort and the NLA (as will be described later), no explicit Boeing NLA data other than that published in the open literature has been used in the conduct of the study reported here.
Document ID
19970003675
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
McMasters, John H.
(Boeing Commercial Airplane Co. Seattle, WA United States)
Paisley, David J.
(Boeing Commercial Airplane Co. Seattle, WA United States)
Hubert, Richard J.
(Boeing Commercial Airplane Co. Seattle, WA United States)
Kroo, Ilan
(Stanford Univ. CA United States)
Bofah, Kwasi K.
(Tuskegee Inst. AL United States)
Sullivan, John P.
(Purdue Univ. West Lafayette, IN United States)
Drela, Mark
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:198351
NASA-CR-201614
D6-81724
Accession Number
97N12363
Funding Number(s)
PROJECT: RTOP 505-90-59-05
CONTRACT_GRANT: NAS1-20269
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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