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A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator

Qineng WANG Zhendong GUO Liming SONG Tianyuan LIU

中国航空学报（英文版）2025，Vol.38Issue(7)：99-114,16.

中国航空学报（英文版）2025，Vol.38Issue(7)：99-114,16.DOI:10.1016/j.cja.2025.103473

A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator

Qineng WANG ¹Zhendong GUO ¹Liming SONG ¹Tianyuan LIU²

作者信息

1. Institute of Turbomachinery,Xi'an Jiaotong University,Xi'an 710049,China
2. ENN Science and Technology Development China Co.,Ltd.,Langfang 065001,China||Hebei Key Laboratory of Compact Fusion,Langfang 065001,China
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摘要

关键词

Turbomachinery/Aerodynamic design/Physics field prediction/Neural networks/Compressor design

Key words

Turbomachinery/Aerodynamic design/Physics field prediction/Neural networks/Compressor design

引用本文复制引用

Qineng WANG,Zhendong GUO,Liming SONG,Tianyuan LIU..A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator[J].中国航空学报（英文版）,2025,38(7):99-114,16.

基金项目

This study was supported by the National Science and Tech-nology Major Project,China(No.2019-Ⅱ-0008-0028). （No.2019-Ⅱ-0008-0028）

中国航空学报（英文版）

ISSN：1000-9361

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