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Application of NASTRAN to TFTR toroidal field coil structuresThe primary applied loads on the TF coils were electromagnetic and thermal. The complex structure and the tremendous applied loads necessitated computer type of solutions for the design problems. In the early stage of the TF coil design, many simplified finite element models were developed for the purpose of investigating the effects of material properties, supporting schemes, and coil case material on the stress levels in the case and in the copper coil. In the more sophisticated models that followed the parametric and scoping studies, the isoparametric elements, such as QUAD4, HEX8, and HEXA, were used. The analysis results from using these finite element models and the NASTRAN system were considered accurate enough to provide timely design information.
Document ID
19780024539
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chen, S. J.
(Ebasco Services, Inc. New York, NY, United States)
Lee, E.
(Grumman Aerospace Corp. Bethpage, N.Y., 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
78N32482
Funding Number(s)
CONTRACT_GRANT: EY-76-C-02-3093
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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