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Inclusion of explicit thermal requirements in optimum structural designA finite-element based procedure is described for obtaining minimum mass designs of structures subjected to combined thermal and mechanical loading and both strength and thermal constraints. The procedure is based on a mathematical programming method using the Sequence of Unconstrained Minimizations Technique (SUMT) in which design requirements are incorporated by an exterior penalty function. The procedure is limited to steady-state temperatures which are controlled by structural sizing only. The optimization procedure is demonstrated by the design of a structural wing box with both mechanical loading and external heating, subject to design constraints on stress, minimum gage, and temperature. The final design for these conditions is compared with a corresponding design in which temperature constraints are omitted.
Document ID
19770014525
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Adelman, H. M.
(NASA Langley Research Center Hampton, VA, United States)
Sawyer, P. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-74017
Report Number: NASA-TM-X-74017
Accession Number
77N21469
Funding Number(s)
PROJECT: RTOP 743-01-11-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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