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A robust study of reliability-based optimization methods under eigen-frequency

机译:特征频率下基于可靠性的优化方法的稳健研究

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Nowadays, the search in reliability-based design optimization is becoming an important engineering design activity. Traditionally for these problems, the objective function is to minimize a cost function while satisfying the reliability constraints. The reliability constraints are usually formulated as constraints on the probability of failure. This paper focuses on the study of a particular problem with the failure mode on vibration of structure. The difficulty in evaluating reliability constraints comes from the fact that modern reliability analysis methods are themselves formulated as an optimization problem. Solving such nested optimization problems is extremely expensive for large-scale multidisciplinary systems which are likewise computationally intensive. With this in mind research, we propose in this paper a new method to treat reliability-based optimization methods under frequencies constraint. The goal of this development has resolved just one problem of optimization and reduced the cost of computation. Aircraft wing design typically involves multiple disciplines such as aerodynamics and structure; this numerical example demonstrated the different advantages of the proposed method.
机译:如今,基于可靠性的设计优化的搜索正成为一项重要的工程设计活动。传统上,对于这些问题,目标功能是在满足可靠性约束的同时最小化成本函数。可靠性约束通常被表述为对故障概率的约束。本文重点研究结构振动失效模式的一个特殊问题。评估可靠性约束的困难来自于这样一个事实,即现代可靠性分析方法本身被公式化为一个优化问题。对于同样计算量大的大规模多学科系统,解决这样的嵌套优化问题非常昂贵。考虑到这一点,本文提出了一种在频率约束下处理基于可靠性的优化方法的新方法。该开发的目标仅解决了一个优化问题并降低了计算成本。飞机机翼设计通常涉及多个学科,例如空气动力学和结构。该数值示例证明了所提出方法的不同优势。

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