CORC  > 北京航空航天大学
Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes
He, Wei; Deng, Qinghua; Zhou, Weilun; Gao, Tieyu; Feng, Zhenping
刊名APPLIED THERMAL ENGINEERING
2019
卷号150页码:150-163
关键词Trenched cooling holes Turbine vane Adiabatic film cooling effectiveness Discharge coefficient Total pressure loss
ISSN号1359-4311
DOI10.1016/j.applthermaleng.2019.01.002
URL标识查看原文
收录类别SCIE ; EI
WOS记录号WOS:000462418200016
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5922353
专题北京航空航天大学
推荐引用方式
GB/T 7714
He, Wei,Deng, Qinghua,Zhou, Weilun,et al. Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes[J]. APPLIED THERMAL ENGINEERING,2019,150:150-163.
APA He, Wei,Deng, Qinghua,Zhou, Weilun,Gao, Tieyu,&Feng, Zhenping.(2019).Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes.APPLIED THERMAL ENGINEERING,150,150-163.
MLA He, Wei,et al."Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes".APPLIED THERMAL ENGINEERING 150(2019):150-163.
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