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Heat Transfer and Flow Structure of a Turbine Blade's Air-cooled Leading Edge Considering Different Hole Shapes and Additional Flow Angles

QIN Runxuan ZHOU Xun WANG Songtao CAI Le

热科学学报（英文版）2024，Vol.33Issue(4)：1421-1442,22.

热科学学报（英文版）2024，Vol.33Issue(4)：1421-1442,22.DOI:10.1007/s11630-024-1958-4

Heat Transfer and Flow Structure of a Turbine Blade's Air-cooled Leading Edge Considering Different Hole Shapes and Additional Flow Angles

QIN Runxuan ¹ZHOU Xun ¹WANG Songtao ¹CAI Le¹

作者信息

1. School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China
折叠

摘要

关键词

film cooling/GE-E3 turbine/rotor blade/conjugate heat transfer/leading edge

Key words

film cooling/GE-E3 turbine/rotor blade/conjugate heat transfer/leading edge

引用本文复制引用

QIN Runxuan,ZHOU Xun,WANG Songtao,CAI Le..Heat Transfer and Flow Structure of a Turbine Blade's Air-cooled Leading Edge Considering Different Hole Shapes and Additional Flow Angles[J].热科学学报（英文版）,2024,33(4):1421-1442,22.

基金项目

This work was supported by the National Science and Technology Major Project of China(2017-Ⅲ-0009-0035). （2017-Ⅲ-0009-0035）

热科学学报（英文版）

OAEI

ISSN：1003-2169

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