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Optimization Strategy for a Shrouded Turbine Blade Using Variable-Complexity Modeling Methodology

机译:可变复杂度建模方法的带罩涡轮叶片优化策略

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摘要

This paper presents the development of a collaborative optimization framework in combination with a variable-complexity modeling technique for the multidisciplinary coupling analysis and design of a shrouded turbine blade. The multidisciplinary optimization design of the shrouded turbine blade involves a high-fidelity detailed computational model and medium-fidelity models, which can become prohibitively expensive. In this investigation, a variable-complexity modeling methodology is introduced, where low-fidelity models and a scaling function are used to approximate the medium-and high-fidelity models through the optimizers in an inner-loop optimization to reduce computational expense. The optimization framework developed includes the collaborative optimization process, parametric modeling of the shrouded turbine blade, fluid-structure interaction solver using arbitrary Lagrangian-Eulerian formulation, an adaptive hexahedral structure mesh generator by establishing virtual blocks and parametric fixed points, and a variable-complexity modeling method combining the multiplicative and additive corrections to manage three levels of fidelity models. On the shrouded turbine-blade design problem, it achieves a feasible optimizer only calling nine high-fidelity analyses. Response surface model variation and cross-validation tests are performed to verify the predictive power of the response surface model in the multidisciplinary design optimization process of the shrouded turbine blade.
机译:本文介绍了协同优化框架的开发,并结合了变量复杂性建模技术,以对带罩涡轮叶片进行多学科耦合分析和设计。罩式涡轮机叶片的多学科优化设计涉及高保真的详细计算模型和中保真模型,这可能会变得非常昂贵。在这项研究中,介绍了一种可变复杂性建模方法,其中在内部循环优化中使用低保真度模型和缩放函数通过优化器对中保真度和高保真度模型进行近似,以减少计算费用。开发的优化框架包括协同优化过程,带罩涡轮叶片的参数化建模,使用任意拉格朗日-欧拉公式的流固耦合求解器,通过建立虚拟块和参数固定点的自适应六面体结构网格生成器以及可变复杂性乘法和加法校正相结合的建模方法来管理三个级别的保真度模型。在笼罩式涡轮叶片设计问题上,它仅需进行九次高保真度分析即可实现可行的优化器。进行了响应面模型变化和交叉验证测试,以验证带罩涡轮叶片的多学科设计优化过程中响应面模型的预测能力。

著录项

  • 来源
    《AIAA Journal》 |2016年第9期|2808-2818|共11页
  • 作者单位

    Beihang Univ, Sch Energy & Power Engn, Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    Beihang Univ, Sch Energy & Power Engn, Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    Beihang Univ, Sch Energy & Power Engn, Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    Aviation Ind Corp China, China Aviat Engine Estab, Beijing 100028, Peoples R China;

    McGill Univ, Min & Mat Engn, Montreal, PQ H3A 0C5, Canada;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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