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Multi-Objective Optimization of Turbine First-Stage Inlet Guide Vane Internal Impingement Cooling Structure Based on NSGA-Ⅱ Algorithm

LIU Yi LI Yiran MA Qiuping LI Xueying REN Jing

热科学学报（英文版）2026，Vol.35Issue(3)：690-700,11.

热科学学报（英文版）2026，Vol.35Issue(3)：690-700,11.DOI:10.1007/s11630-026-2256-0

Multi-Objective Optimization of Turbine First-Stage Inlet Guide Vane Internal Impingement Cooling Structure Based on NSGA-Ⅱ Algorithm

LIU Yi ¹LI Yiran ¹MA Qiuping ¹LI Xueying ¹REN Jing¹

作者信息

1. Department of Energy and Power Engineering,Tsinghua University,Beijing 100083,China
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摘要

关键词

air-cooled turbine vane/impingement cooling/CFD/surrogate model/multi-objective optimization

Key words

air-cooled turbine vane/impingement cooling/CFD/surrogate model/multi-objective optimization

引用本文复制引用

LIU Yi,LI Yiran,MA Qiuping,LI Xueying,REN Jing..Multi-Objective Optimization of Turbine First-Stage Inlet Guide Vane Internal Impingement Cooling Structure Based on NSGA-Ⅱ Algorithm[J].热科学学报（英文版）,2026,35(3):690-700,11.

基金项目

This research is funded by the National Science and Technology Major Project(No.J2019-Ⅲ-0007-0050)and National Science and Technology Major Project(No.Y2022-Ⅲ-0003-0012). （No.J2019-Ⅲ-0007-0050）

热科学学报（英文版）

ISSN：1003-2169

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