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Toward a second generation fuel efficient supersonic cruise aircraft structural design for efficiencyThe unique challenge of this concept to the structural designer is discussed. The potential of the application of advanced structural design concepts and new titanium fabrication processes is emphasized. Highlighted are the results of a detailed structural analysis, including weight and flutter, showing successful use of the ATLAS structural design and analysis system. It is concluded that blending of the structure may not have an adverse impact on structural efficiency, weight, and manufacturing complexity.
Document ID
19770011094
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoy, J. R.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Proc. of the SCAR Conf., Pt. 2,
Subject Category
Aircraft Design, Testing And Performance
Accession Number
77N18038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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