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Mixed time integration methods for transient thermal analysis of structures, appendix 5Mixed time integration methods for transient thermal analysis of structures are studied. An efficient solution procedure for predicting the thermal behavior of aerospace vehicle structures was developed. A 2D finite element computer program incorporating these methodologies is being implemented. The performance of these mixed time finite element algorithms can then be evaluated employing the proposed example problem.
Document ID
19830012012
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Liu, W. K.
(Northwestern Univ. Evanston, IL, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-170061
NAS 1.26:170061
Report Number: NASA-CR-170061
Report Number: NAS 1.26:170061
Accession Number
83N20283
Funding Number(s)
CONTRACT_GRANT: NAG1-210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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