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Thermal stress analysis of symmetric shells subjected to asymmetric thermal loadsThe performance of the NASTRAN level 16.0 axisymmetric solid elements when subjected to both symmetric and asymmetric thermal loading was investigated. A ceramic radome was modeled using both the CTRAPRG and the CTRAPAX elements. The thermal loading applied contained severe gradients through the thickness of the shell. Both elements were found to be more sensitive to the effect of the thermal gradient than to the aspect ratio of the elements. Analysis using the CTRAPAX element predicted much higher thermal stresses than the analysis using the CTRAPRG element, prompting studies of models for which theoretical solutions could be calculated. It was found that the CTRAPRG element solutions were satisfactory, but that the CTRAPAX element was very geometry dependent. This element produced erroneous results if the geometry was allowed to vary from a rectangular cross-section. The most satisfactory solution found for this type of problem was to model a small segment of a symmetric structure with isoparametric solid elements and apply the cyclic symmetry option in NASTRAN.
Document ID
19800016159
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Negaard, G. R.
(Anamet Labs., Inc. Berkeley, CA, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Eighth NASTRAN User's Colloq.
Subject Category
Structural Mechanics
Accession Number
80N24652
Funding Number(s)
CONTRACT_GRANT: F33615-77-C-3046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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