Titlebook: Discretization Methods and Structural Optimization — Procedures and Applications; Proceedings of a GAM Hans A. Eschenauer,Georg Thierauf Co

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Muhittin Onur Akca,Osman Sonmeze principal goal of this paper is to show the integration of information from the domain of manufacturing (including material selection) and simple analysis techniques in preliminary design. This is effectively accomplished within the framework of the Decision Support Problem Technique by formulating and solving coupled decision support problems.

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https://doi.org/10.1007/978-3-642-83707-4algorithm; algorithms; calculus; finite element method; linear optimization; mathematical programming; mec

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978-3-540-50784-0Springer-Verlag Berlin, Heidelberg 1989

GREG

Shape Optimization as a Discrete Optimization Problem — Solution Procedures Using Continuous Approxior no material. Various ways of attacking this general problem by use of layered materials and porous, periodic media are presented and it is illustrated that the method allows a determination of the topology of a mechanical element.

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Application of Interactive Vector Optimization Methods with Regard to Problems in Structural Mechaniaking. These procedures can also be applied on structural and component optimization problems as shown in the following. The non-linearity of the optimization problem, time-consuming analytical or numerical structural analyses and the limited validity of the optimization model provide higher demands on the interactive procedure.

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Preliminary Design of a Filament Wound Pressure Vessel: A Coupled Decision Support Probleme principal goal of this paper is to show the integration of information from the domain of manufacturing (including material selection) and simple analysis techniques in preliminary design. This is effectively accomplished within the framework of the Decision Support Problem Technique by formulating and solving coupled decision support problems.

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Hallowed

Melodrama

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Soils and Sustainable Agriculture: A Reviewnly in some lack of generality and flexibility of computer software and the relatively high computational effort envolved. This is especially true when problems are governed by considerations in structural dynamics, which is the case for structural design of most spacecraft structures where often st