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NASTRAN finite element idealization studyThe investigation of the effects of variations of mesh refinement and mesh pattern were conducted using a basic rectangular mesh pattern. When employing the constant strain TRMEM element, the basic rectangular pattern was subdivided into triangles. This subdivision employs two different triangular patterns and allows results to be obtained which demonstrate the effect of modelling bias. Errors in tip deflection, direct stress, and shearing stress as a function of mesh size and element aspect ratio were obtained as well as mid-span stress distributions. All problems were solved on an IBM 360/95 computer using MacNeal-Schwendler Version MSC-38 Rigid Format-1 of the NASTRAN computer program. While NASTRAN uses double precision arithmetic for the solution of the global equations for displacements, subsequent computations to obtain element stresses are carried out in single precision. This suggests that some improvement in stress recovery might be expected when using the higher precision DCD machines.
Document ID
19780004525
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Case, W. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mason, J. B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA, Washington 6th NASTRAN (R) Users' Colloq.
Subject Category
Structural Mechanics
Accession Number
78N12468
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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