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Effects of Ribbed-Cavity Tip on the Blade Tip Aerothermal Performance in a High Pressure Turbine Stage

DU Kun LI Huarong SUNDEN Bengt LIU Cunliang

热科学学报:英文版2023,Vol.32Issue(2):P.800-811,12.
热科学学报:英文版2023,Vol.32Issue(2):P.800-811,12.DOI:10.1007/s11630-023-1771-5

Effects of Ribbed-Cavity Tip on the Blade Tip Aerothermal Performance in a High Pressure Turbine Stage

DU Kun 1LI Huarong 1SUNDEN Bengt 1LIU Cunliang1

作者信息

  • 折叠

摘要

关键词

gas turbine/tip leakage flow/numerical simulation/blade tip configuration

分类

航空航天

引用本文复制引用

DU Kun,LI Huarong,SUNDEN Bengt,LIU Cunliang..Effects of Ribbed-Cavity Tip on the Blade Tip Aerothermal Performance in a High Pressure Turbine Stage[J].热科学学报:英文版,2023,32(2):P.800-811,12.

基金项目

the support of National Natural Science Foundation of China(No.52006178,51936008) (No.52006178,51936008)

National Key R&D Program of China(No.Y2019-Ⅷ-0007-0168) (No.Y2019-Ⅷ-0007-0168)

the Fundamental Research Funds for the Central Universities ()

the Innovation Capacity Support Plan in Shaanxi Province of China(Grant No.2023-CX-TD-19)。 (Grant No.2023-CX-TD-19)

热科学学报:英文版

OACSCDEI

1003-2169

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