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NASTRAN buckling analysis of a thin walled cylinderThe computer run time required for a buckling analysis using NASTRAN is considerably greater than for a linear static analysis of the same structure. It is very important to obtain an optimal model size for the structure being analyzed, such that the model is neither so large as to increase running time unnecessarily, nor so small as to hinder accuracy. The problem of critical load accuracy versus model complexity is considered for a thin walled cylinder, using both Level 12 and Level 15 NASTRAN releases.
Document ID
19720025222
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wight, R. B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Publication Information
Publication: NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
72N32872
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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