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RELIABILITY-BASED OPTIMAL STRUCTURAL AND MECHANICAL DESIGN.

机译:基于可靠性的最佳结构和机械设计。

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Structural reliability technology provides analytical tools for management of uncertainty in all relevant design factors in structural and mechanical systems. Generally, the goal of analysis is to compute probabilities of failure in structural components or system having single or multiple failure mode. Alternately, modern optimization methods provide efficient numerical algorithms for locating optima, particularly in large-scale systems having prescribed deterministic constraints. Optimization procedure can accommodate random variables either directly in its objective function or as one of the primary constraints. The combination of elementary optimization and probabilistic design techniques is the subject of this study. Presented herein is a general strategy for optimization when the design factors are random variables and some or all of the constraints are probability statements.; A literature review has indicated that optimization technology in a reliability context has not been fully explored for the general case of nonlinear performance functions and nonnormal variates associated multiple failure modes. This research focuses upon development of the theory to address this general problem. Because analysis algorithms are complicated, a computer code, program RELOPT, is constructed to automate the analysis.; The objective function to be minimized is arbitrary, but would generally be the total expected lifetime costs including all initial costs as well as all costs associated with failure. Uncertainty is assumed to be possible in all design factors (including the factors to be determined), and they are modeled as random variables. In general, all of the constraints can be probability statements. The generalized reduce gradient (GRG) method was used for optimization calculations. Options for point probability calculations are first order reliability analysis using the Rackwitz-Fiessler (R-F) or advanced reliability analysis using Wu/FPI. For system reliability analysis either the first order Cornell's bounds or the second order Ditlevsen's bounds can be specified.; Several examples are presented to illustrate the full range of capabilities of RELOPT. The program is validated by checking with independent and exact solutions. An example is provided which demonstrates that the cost of running RELOPT can be substantial as the size of the problem increases.
机译:结构可靠性技术为分析结构和机械系统中所有相关设计因素的不确定性提供了分析工具。通常,分析的目的是计算具有单个或多个故障模式的结构组件或系统中的故障概率。可替代地,现代优化方法提供了用于定位最优的有效数值算法,特别是在具有规定确定性约束的大规模系统中。优化过程可以直接在其目标函数中或作为主要约束之一来容纳随机变量。基本优化和概率设计技术的结合是本研究的主题。当设计因子是随机变量并且某些或所有约束是概率陈述时,本文提出了一种优化的一般策略。文献综述表明,对于非线性性能函数和与多种故障模式相关的非正态变量的一般情况,尚未充分探索可靠性环境中的优化技术。这项研究致力于解决这一普遍问题的理论的发展。因为分析算法很复杂,所以构建了计算机代码RELOPT来自动执行分析。要最小化的目标函数是任意的,但通常是预期的总寿命成本,包括所有初始成本以及与故障相关的所有成本。假定所有设计因素(包括待确定的因素)中都存在不确定性,并且将它们建模为随机变量。通常,所有约束都可以是概率陈述。通用归约梯度(GRG)方法用于优化计算。点概率计算的选项是使用Rackwitz-Fiessler(R-F)进行一阶可靠性分析或使用Wu / FPI进行高级可靠性分析。对于系统可靠性分析,可以指定一阶康奈尔边界或二阶Ditlevsen边界。提供了一些示例来说明RELOPT的全部功能。通过使用独立且准确的解决方案进行检查来验证该程序。提供了一个示例,说明随着问题规模的增加,运行RELOPT的成本可能会很高。

著录项

  • 作者

    LEE, SEUNG JOO.;

  • 作者单位

    The University of Arizona.;

  • 授予单位 The University of Arizona.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1987
  • 页码 208 p.
  • 总页数 208
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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