NASA NTRS ยท 19740006478
NASTRAN static and buckling analysis - comparison with other large-capacity programs
Abstract
A 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.
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Shah, L. C.. 1973-09-01. NASTRAN static and buckling analysis - comparison with other large-capacity programs. https://ntrs.nasa.gov/citations/19740006478
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