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A high-fidelity design methodology using LES-based simulation and POD-based emulation:A case study of swirl injectors

机译:一种基于LES的仿真和基于POD的仿真的高保真设计方法:以旋流喷油器为例

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摘要

Engineering design is undergoing a paradigm shift from design for performance to design for affordability, operability, and durability, seeking multi-objective optimization. To facilitate this transformation, significantly extended design freedom and knowledge must be available in the early design stages. This paper presents a high-fidelity framework for design and optimization of the liq-uid swirl injectors that are widely used in aerospace propulsion and power-generation systems. The framework assembles a set of techniques, including Design Of Experiment (DOE), high-fidelity Large Eddy Simulations (LES), machine learning, Proper Orthogonal Decomposition (POD)-based Kriging surrogate modeling (emulation), inverse problem optimization, and uncertainty quantification. LES-based simulations can reveal detailed spatiotemporal evolution of flow struc-tures and flame dynamics in a high-fidelity manner, and identify important injector design param-eters according to their effects on propellant mixing, flame stabilization, and thermal protection. For a given a space of design parameters, DOE determines the number of design points to perform LES-based simulations. POD-based emulations, trained by the LES database, can effectively explore the design space and deduce an optimal group of design parameters in a turn-around time that is reduced by three orders of magnitude. The accuracy of the emulated results is validated, and the uncertainty of prediction is quantified. The proposed design methodology is expected to pro-foundly extend the knowledge base and reduce the cost for initial design stages.
机译:工程设计正在经历从性能设计到价格可承受性,可操作性和耐用性设计的范式转变,以寻求多目标优化。为了促进这种转变,在早期设计阶段必须提供显着扩展的设计自由和知识。本文提出了一种用于设计和优化液体旋流喷油器的高保真框架,该旋流喷油器广泛用于航空航天推进和发电系统。该框架集合了一系列技术,包括实验设计(DOE),高保真大型涡流仿真(LES),机器学习,基于正确正交分解(POD)的克里格代理模型(仿真),逆问题优化和不确定性量化。基于LES的模拟可以高保真地揭示流动结构和火焰动力学的详细时空演变,并根据其对推进剂混合,火焰稳定和热保护的影响来确定重要的喷射器设计参数。对于给定的设计参数空间,DOE确定执行基于LES的仿真的设计点数。由LES数据库训练的基于POD的仿真可以有效地探索设计空间并在减少三个数量级的周转时间内得出一组最佳的设计参数。验证了仿真结果的准确性,并对预测的不确定性进行了量化。预期所提出的设计方法将大大扩展知识库并降低初始设计阶段的成本。

著录项

  • 来源
    《中国航空学报(英文版)》 |2018年第9期|1855-1869|共15页
  • 作者单位

    School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332, USA;

    School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332, USA;

    School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332, USA;

    School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332, USA;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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