Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
|更新时间:2026-07-07
|
Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
Vol. 25, Issue 4, (2010)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国航空工业集团公司 中国航空动力机械研究所,株洲,412002
作者简介:
基金信息:
DOI:
CLC:
Published:2010
稿件说明:
移动端阅览
YANG Wei-hua, WANG Mei-juan, DING You-hong, et al. Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling[J]. 2010, 25(4).
DOI:
YANG Wei-hua, WANG Mei-juan, DING You-hong, et al. Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling[J]. 2010, 25(4).DOI:
Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
In order to study the heat transfer characteristics of impingement/cocurrent convection/film double cooling
several test pieces were designed.The experimental results show that the cooling efficiency increases with the growing blowing ratio;the distribution of cooling efficiency is wavy on the cooling wall.The cooling efficiency is higher in the areas of cooling film exit and the impingement stagnant point.The decrease of cooling efficiency is weakened behind the impingement stagnant point.Cooling efficiency increases with the decrease of impingement space.
Experimental study of the heat transfer characteristics of combined cooling of impingement+reversed convection+film
Numerical computation and analysis of three-dimensional wall temperature of impingement+identical flow convection+film composite cooling
Thermal fatigue behavior of nickle based superalloy GH536
Experiment of cooling effectiveness with double-outlet film hole
Performance comparative experiment on flame tubes of a certain combustor
Related Author
SONG Shuang-wen
YANG Wei-hua
HU Hao-sheng
SONG Shuang-wen
HU Hao-sheng
PENG Jian-yong
陈静
石多奇
Related Institution
China Aviatio n Powerplant Research Instit ute, Zhuzho u
北京航空航天大学 能源与动力工程学院
先进航空发动机协同创新中心
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
School of Power and Energy,Northwestern Polytechnical University