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
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)