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NASTRAN static and buckling analysis - comparison with other large-capacity programsA square plate with clamped edges under a concentrated load was modeled using NASTRAN and ASKA finite element computer programs. Deflections were computed for various width-to-thickness ratios (b/t) of the plate element, and were compared against the classical theory to determine the b/t limitations. A cylinder with simply supported ends was modeled using NASTRAN and STAGS computer programs for buckling analysis. The models were subjected to a uniform radial pressure loading. Several parameters were changed, and the effects of those variations are presented. Utilizing these data, a model which will produce results comparable to published empirical data can be constructed and processed for a minimized cost.
Document ID
19740006478
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shah, L. C.
(Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Langley Res. Center NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
74N14591
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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