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Experimental and Numerical Investigation on Cooling and Aerodynamic Performance of Turbine Blade Ribbed Squealer Tip

LIU Zhao JIA Zhe XU Yao FENG Zhenping

热科学学报（英文版）2025，Vol.34Issue(3)：819-833,15.

热科学学报（英文版）2025，Vol.34Issue(3)：819-833,15.DOI:10.1007/s11630-025-2026-4

Experimental and Numerical Investigation on Cooling and Aerodynamic Performance of Turbine Blade Ribbed Squealer Tip

LIU Zhao ¹JIA Zhe ¹XU Yao ¹FENG Zhenping¹

作者信息

1. Institute of Turbomachinery,Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment,School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China
折叠

摘要

关键词

tip structures/film cooling/aerodynamic loss/gas turbine

Key words

tip structures/film cooling/aerodynamic loss/gas turbine

引用本文复制引用

LIU Zhao,JIA Zhe,XU Yao,FENG Zhenping..Experimental and Numerical Investigation on Cooling and Aerodynamic Performance of Turbine Blade Ribbed Squealer Tip[J].热科学学报（英文版）,2025,34(3):819-833,15.

基金项目

This work was supported by the National Science and Technology Major Project(J2019-Ⅲ-0007-0050). （J2019-Ⅲ-0007-0050）

热科学学报（英文版）

ISSN：1003-2169

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