Prediction of multi-physics field distribution on gas turbine endwall using an optimized surrogate model with various deep learning frames

被引:2
作者
Zhang, Weixin [1 ]
Liu, Zhao [1 ]
Song, Yu [1 ]
Lu, Yixuan [1 ]
Feng, Zhenping [1 ]
机构
[1] Xi An Jiao Tong Univ, Inst Turbomachinery, Sch Energy & Power Engn, Shaanxi Engn Lab Turbomachinery & Power Equipment, Xian, Peoples R China
关键词
Surrogate model; Data driven; Prediction; Gas turbine; Film cooling; FILM-COOLING EFFECTIVENESS; VANE ENDWALL; DESIGN; TURBOMACHINERY; ROWS;
D O I
10.1108/HFF-10-2023-0620
中图分类号
O414.1 [热力学];
学科分类号
摘要
PurposeTo improve the speed and accuracy of turbine blade film cooling design process, the most advanced deep learning models were introduced into this study to investigate the most suitable define for prediction work. This paper aims to create a generative surrogate model that can be applied on multi-objective optimization problems.Design/methodology/approachThe latest backbone in the field of computer vision (Swin-Transformer, 2021) was introduced and improved as the surrogate function for prediction of the multi-physics field distribution (film cooling effectiveness, pressure, density and velocity). The basic samples were generated by Latin hypercube sampling method and the numerical method adopt for the calculation was validated experimentally at first. The training and testing samples were calculated at experimental conditions. At last, the surrogate model predicted results were verified by experiment in a linear cascade.FindingsThe results indicated that comparing with the Multi-Scale Pix2Pix Model, the Swin-Transformer U-Net model presented higher accuracy and computing speed on the prediction of contour results. The computation time for each step of the Swin-Transformer U-Net model is one-third of the original model, especially in the case of multi-physics field prediction. The correlation index reached more than 99.2% and the first-order error was lower than 0.3% for multi-physics field. The predictions of the data-driven surrogate model are consistent with the predictions of the computational fluid dynamics results, and both are very close to the experimental results. The application of the Swin-Transformer model on enlarging the different structure samples will reduce the cost of numerical calculations as well as experiments.Research limitations/implicationsThe number of U-Net layers and sample scales has a proper relationship according to equation (8). Too many layers of U-Net will lead to unnecessary nonlinear variation, whereas too few layers will lead to insufficient feature extraction. In the case of Swin-Transformer U-Net model, incorrect number of U-Net layer will reduce the prediction accuracy. The multi-scale Pix2Pix model owns higher accuracy in predicting a single physical field, but the calculation speed is too slow. The Swin-Transformer model is fast in prediction and training (nearly three times faster than multi Pix2Pix model), but the predicted contours have more noise. The neural network predicted results and numerical calculations are consistent with the experimental distribution.Originality/valueThis paper creates a generative surrogate model that can be applied on multi-objective optimization problems. The generative adversarial networks using new backbone is chosen to adjust the output from single contour to multi-physics fields, which will generate more results simultaneously than traditional surrogate models and reduce the time-cost. And it is more applicable to multi-objective spatial optimization algorithms. The Swin-Transformer surrogate model is three times faster to computation speed than the Multi Pix2Pix model. In the prediction results of multi-physics fields, the prediction results of the Swin-Transformer model are more accurate.
引用
收藏
页码:2865 / 2889
页数:25
相关论文
共 44 条
  • [1] Alshehaby M.M., 2019, IMECE C P 2019, DOI [10.1115/IMECE2019-10974, DOI 10.1115/IMECE2019-10974]
  • [2] Alshehaby M.M., 2017, ASME C P 2017, DOI [10.1115/GT2017-65063, DOI 10.1115/GT2017-65063]
  • [3] Anderson JB, 2016, PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5C
  • [4] Correlation of film-cooling effectiveness from thermographic measurements at enginelike conditions
    Baldauf, S
    Scheurlen, M
    Schulz, A
    Wittig, S
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2002, 124 (04): : 686 - 698
  • [5] Cao H., 2017, ARXIV
  • [6] Surrogate-based optimization and experiment validation of a fan-shaped film cooling hole with a large lateral space
    Chen Liu
    Bao Amei
    Zhang Yi
    Chen Dawei
    Guan Junjun
    Dai Ren
    [J]. APPLIED THERMAL ENGINEERING, 2022, 207
  • [7] Optimization of film cooling arrays on a gas turbine vane by using an integrated approach of numerical simulation and parameterized design
    Dong, Ziyu
    Liu, Daoyin
    Liang, Cai
    Hao, Menglong
    Dai, Ting
    Ding, Hui
    [J]. APPLIED THERMAL ENGINEERING, 2023, 219
  • [8] Aerodynamic design and optimization of blade end wall profile of turbomachinery based on series convolutional neural network
    Du, Qiuwan
    Yang, Like
    Li, Liangliang
    Liu, Tianyuan
    Zhang, Di
    Xie, Yonghui
    [J]. ENERGY, 2022, 244
  • [9] Optimizing the trench shaped film cooling design
    Fischer, Lukas
    James, Dominik
    Jeyaseelan, Sillvya
    Pfitzner, Michael
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2023, 214
  • [10] Prediction of aerodynamic and thermal performances for gas foil journal bearing with an axial cooling throughflow by machine learning method
    Gao, Qi-hong
    Sun, Wen-jing
    Zhang, Jing-zhou
    [J]. THERMAL SCIENCE AND ENGINEERING PROGRESS, 2023, 44