您当前的位置:
首页 >
文章列表页 >
Influence of coolant crossflow on film cooling effectiveness of one-inlet and double-outlet injection holes
更新时间:2025-09-28
    • Influence of coolant crossflow on film cooling effectiveness of one-inlet and double-outlet injection holes

    • Thermal Power Generation   Issue 2, (2016)
    • CLC: TK47
    • Published Online:15 March 2016,

      Published:2016

    移动端阅览

  • ZHANG Wei, LI Guangchao, KOU Zhihai, et al. Influence of coolant crossflow on film cooling effectiveness of one-inlet and double-outlet injection holes[J]. Thermal power generation, 2016, (2). DOI:

  •  
  •  

0

Views

254

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Investigation on film cooling effectiveness of fanned hole with broad outlet
Experimental investigation of film cooling efficiency on turbine blade surface with one-inlet and double-outlet hole injection
Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins
Effects of attack angle and endwall slippage on flow and heat transfer of blade squealer tip

Related Author

LI Guangchao
PENG Ningjian
ZHANG Wei
KOU Zhihai
MAO Xiaodong
ZHANG Guochen
LI Guangchao
CHEN Yukai

Related Institution

Liaoning Key Lab of Advanced Measurement and Test Technique for Aviation Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
Liaoning Key Lab of Advanced Test and Measurement for Aviation Propulsion System,Shenyang Aerospace University
Liaoning Province Key Laboratory of Advanced Testing Technology for Aerospace Propulsion Systems, Shenyang University of Aeronautics and Astronautics
China Gas Turbine Research Institute of Aviation Industry Corporation of China
Liaoning Key Lab of Advanced Measurement and Test Technology for Aviation Propulsion System,Faculty of Aerospace Engineering,Shenyang Aerospace University Shenyang
0