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Structural analysis for preliminary design of High Speed Civil Transport (HSCT)In the preliminary design environment, there is a need for quick evaluation of configuration and material concepts. The simplified beam representations used in the subsonic, high aspect ratio wing platform are not applicable for low aspect ratio configurations typical of supersonic transports. There is a requirement to develop methods for efficient generation of structural arrangement and finite element representation to support multidisciplinary analysis and optimization. In addition, empirical data bases required to validate prediction methods need to be improved for high speed civil transport (HSCT) type configurations.
Document ID
19920016683
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bhatia, Kumar G.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Computational Structures Technology for Airframes and Propulsion Systems
Subject Category
Structural Mechanics
Accession Number
92N25926
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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