A NOVEL MULTI-FIDELITY SURROGATE FOR TURBOMACHINERY DESIGN OPTIMIZATION

被引:0
作者
Wang, Qineng [1 ]
Song, Liming [1 ]
Guo, Zhendong [1 ]
Li, Jun [1 ]
Feng, Zhenping [1 ]
机构
[1] Xi An Jiao Tong Univ, Inst Turbomachinery, Xian, Peoples R China
来源
PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13D | 2023年
关键词
Turbomachinery design; Multi-fidelity surrogate; Surrogate-based optimization; Ensemble modeling; SCALE FACTOR; SIMULATION;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The design optimization of turbomachinery is a challenging task as it involves expensive black-box problems. The sample-efficient multi-fidelity optimization (MFO) algorithm has been proposed as an efficient solution to this problem. By utilizing multi-fidelity surrogates (MFS), the MFO algorithm can use fewer high-fidelity samples aided by low-fidelity samples to establish an accurate surrogate model. However, when MFS is used in sequential sampling optimization, it has been observed that the final optimal solution obtained by single-fidelity optimization (SFO) is better than that of MFO, even though MFO performs better at the early stages. This can be attributed to the assumption of an even and nested distribution of samples, which is incorrect when using a sequential adding strategy. To address these issues, we propose a novel algorithm called multi-single-fidelity optimization (MSFO) to overcome the limitations of the conventional MFO procedures. In the surrogate establishment of MSFO, we use the density-based spatial clustering of applications with noise (DBSCAN) method to detect local areas where low-fidelity samples are no longer effective. A combination of both global MFS and local single-fidelity surrogate model, built using high-fidelity samples alone, is used to establish an ensemble, which improves the anti-interference ability of the algorithm against misleading low-fidelity data. The effectiveness of the MSFO algorithm is verified first on numerical benchmark functions. Then, the algorithm is used to optimize the aerodynamic profile of a turbine and the film cooling layout design of a turbine endwall. Here, high-fidelity sample sources are obtained from fine-mesh CFD simulations, whereas low-fidelity sample sources are obtained from the same simulations run on a coarser mesh. The results demonstrate that our MSFO algorithm performs significantly better than the conventional SFO and MFO processes, with a higher level of robustness. Therefore, the effectiveness of the MSFO algorithm is well demonstrated.
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页数:10
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