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Multilevel computer-aided optimum design of structural systems using multiple basis vectors.

机译:使用多个基向量的多层计算机辅助结构系统的优化设计。

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摘要

A new alternative multilevel structural optimization method using multiple basis vectors for each substructure is presented. The system level design task is formulated using multiple design space basis vectors for each substructure and the corresponding participation coefficients (system level design variables). In the system level design problem the total structural weight is minimized, subject to the system level constraints, namely static displacement limitations and natural frequency constraints. At the end of a system level optimization stage, the weight of each substructure is evaluated and used to establish an updated upper bound weight cap constraint for each upcoming substructure optimization procedure. At the subsystem level the structure is decomposed into a number of small substructures each one of which contains multiple design space basis vectors. A buffer (slack) variable is selected as the objective function for each substructure. Stress and member buckling constraints are incorporated at the subsystem level. The design modification problem at the subsystem level is formulated in a manner such that maximization of the buffer variable drives the substructure design vector away from all of the constraints except the side constraints. After completing the subsystem level optimization task, the final values of buffer variables, local behavior constraints, and local design variables are obtained and used to evaluate lower limit values for the upcoming system level design variables. At both the system level and the subsystem level, design modification is carried out by solving a sequence of explicit approximate problems. The new alternative multilevel method which introduces multiple basis vectors for each substructure leads to greater flexibility when constructing and solving design optimization models for large structural systems.
机译:提出了一种新的替代性多级结构优化方法,该方法对每个子结构使用多个基向量。使用每个子结构的多个设计空间基础向量和相应的参与系数(系统级设计变量)来制定系统级设计任务。在系统级设计问题中,受制于系统级约束,即静态位移约束和固有频率约束,使总结构重量最小化。在系统级优化阶段的最后,评估每个子结构的权重,并将其用于为每个即将到来的子结构优化过程建立更新的上限权重上限约束。在子系统级别,结构分解为许多小的子结构,每个子结构都包含多个设计空间基础向量。选择一个缓冲区(松弛)变量作为每个子结构的目标函数。应力和构件屈曲约束纳入子系统级别。子系统级别的设计修改问题以这样的方式提出:缓冲变量的最大化驱使子结构设计矢量远离除侧面约束之外的所有约束。完成子系统级别的优化任务后,将获得缓冲区变量,局部行为约束和局部设计变量的最终值,并将其用于评估即将到来的系统级设计变量的下限值。在系统级别和子系统级别,都通过解决一系列显式近似问题来进行设计修改。在为大型结构系统构建和求解设计优化模型时,新的替代性多级方法为每个子结构引入了多个基向量,从而带来了更大的灵活性。

著录项

  • 作者

    Seomun, Kang-Seon.;

  • 作者单位

    University of California, Los Angeles.;

  • 授予单位 University of California, Los Angeles.;
  • 学科 Aerospace engineering.;Automotive engineering.;Mechanical engineering.
  • 学位 Ph.D.
  • 年度 1992
  • 页码 312 p.
  • 总页数 312
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:50:16

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