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NASA NTRS ยท 19750022522

Design of structures for optimum geometry

Abstract

A 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.

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BibTeXRIS

Vanderplaats, G. N.. 1975-08-01. Design of structures for optimum geometry. https://ntrs.nasa.gov/citations/19750022522

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