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Design of structures for optimum geometryA method is presented for configuration optimization of finite element structures, given a reasonable initial geometry. The objective is to minimize weight or cost. Design variables include geometric as well as member sizing parameters. The number of elements and joints, and the element-joint relationships are prescribed and are not changed during the optimization process. However, the joint locations are changed. The structure is assumed to be linearly elastic and may be statically indeterminate. Multiple loading conditions are allowed. Constraints include limits on stiffness as well as strength. The method is demonstrated with application to truss design, subject to minimum size, strength, buckling, and displacement constraints. Major design improvements are achieved through configurations changes.
Document ID
19750022522
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vanderplaats, G. N.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-62462
A-6204
Report Number: NASA-TM-X-62462
Report Number: A-6204
Accession Number
75N30595
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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