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NASTRAN applications to aircraft propulsion systemsThe use of NASTRAN in propulsion system structural integration analysis is described. Computer support programs for modeling, substructuring, and plotting analysis results are discussed. Requirements on interface information and data exchange by participants in a NASTRAN substructure analysis are given. Static and normal modes vibration analysis results are given with comparison to test and other analytical results.
Document ID
19750023418
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
White, J. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Beste, D. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1975
Publication Information
Publication: NASA. Langley Res. Center NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
75N31491
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19750023412Collected WorksNASTRAN: User's Experiences
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