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A simple element for multilayer beams in NASTRAN thermal stress analysisIn the application of NASTRAN, structural members are usually represented by bar elements with multipoint constraint cards to enforce the interface conditions. While this is a very powerful method in principle, it was found that in practice the process for specification of constraints became tedious and error prone, unless the geometry was simple and the number of grid points low. An alternative approach was found within the framework of the NASTRAN program. This approach made use of the idea that a thermal distortion in a multilayer beam may be similar to a homogeneous beam with a thermal gradient across the cross section. The exact mathematical derivation for the equivalent beam, and all the necessary formulae for the equivalent parameters in NASTRAN analysis are presented. Some numerical examples illustrate the simplicity and ease of this approach for finite element analysis.
Document ID
19780024537
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chen, W. T.
(International Business Machines Corp. Armonk, NY, United States)
Wadhwa, S. K.
(International Business Machines Corp. Armonk, NY, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA. Marshall Space Flight Center Seventh NASTRAN User's Colloq.
Subject Category
Structural Mechanics
Accession Number
78N32480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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