热科学学报（英文版）2010，Vol.19Issue(5)：430-437,8.DOI:10.1007/s11630-010-0405-x
Improving Film Cooling Performance by Using One -Inlet and Double-Outlet Hole
Improving Film Cooling Performance by Using One -Inlet and Double-Outlet Hole
Guang-chao Li 1Wei Zhang1
作者信息
- 1. Aeroengine and Energy Engineering College,Shenyang Areospace University Shenyang China 110136
- 折叠
摘要
关键词
aerospace propulsion system/gas turbine/film cooling/heat transferKey words
aerospace propulsion system/gas turbine/film cooling/heat transfer引用本文复制引用
Guang-chao Li,Wei Zhang..Improving Film Cooling Performance by Using One -Inlet and Double-Outlet Hole[J].热科学学报（英文版）,2010,19(5):430-437,8.
