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Mixed time integration methods for transient thermal analysis of structuresThe computational methods used to predict and optimize the thermal structural behavior of aerospace vehicle structures are reviewed. In general, two classes of algorithms, implicit and explicit, are used in transient thermal analysis of structures. Each of these two methods has its own merits. Due to the different time scales of the mechanical and thermal responses, the selection of a time integration method can be a different yet critical factor in the efficient solution of such problems. Therefore mixed time integration methods for transient thermal analysis of structures are being developed. The computer implementation aspects and numerical evaluation of these mixed time implicit-explicit algorithms in thermal analysis of structures are presented. A computationally useful method of estimating the critical time step for linear quadrilateral element is also given. Numerical tests confirm the stability criterion and accuracy characteristics of the methods. The superiority of these mixed time methods to the fully implicit method or the fully explicit method is also demonstrated.
Document ID
19830011536
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
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-170060
NAS 1.26:170060
Report Number: NASA-CR-170060
Report Number: NAS 1.26:170060
Accession Number
83N19807
Funding Number(s)
CONTRACT_GRANT: NAG1-210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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