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Structural optimization by multilevel decompositionA method is described for decomposing an optimization problem into a set of subproblems and a coordination problem which preserves coupling between the subproblems. The method is introduced as a special case of multilevel, multidisciplinary system optimization and its algorithm is fully described for two level optimization for structures assembled of finite elements of arbitrary type. Numerical results are given for an example of a framework to show that the decomposition method converges and yields results comparable to those obtained without decomposition. It is pointed out that optimization by decomposition should reduce the design time by allowing groups of engineers, using different computers to work concurrently on the same large problem.
Document ID
19830012661
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sobieszczanski-Sobieski, J.
(NASA Langley Research Center Hampton, VA, United States)
James, B.
(Kentron International, Inc. Hampton, VA, United States)
Dovi, A.
(NASA Langley Research Center)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-84641
NAS 1.15:84641
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS 24th Struct., Struct. Dyn. and Mater. Conf.
Location: Lake Tahoe, NV
Country: United States
Start Date: May 2, 1983
End Date: May 4, 1983
Accession Number
83N20932
Funding Number(s)
PROJECT: RTOP 505-33-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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