Experimental study on film cooling characteristics of lamilloy at different blowing ratios
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Experimental study on film cooling characteristics of lamilloy at different blowing ratios
Thermal Power GenerationVol. 44, Issue 9, Pages: 43-47(2015)
作者机构:
1. 沈阳航空航天大学辽宁省航空推进系统先进测试技术重点实验室
2. 中国航空工业集团公司沈阳发动机设计研究所
作者简介:
基金信息:
DOI:
CLC:TK471
Published:2015
稿件说明:
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LI Guangchao, CAO Xifeng, LIU Yongquan, et al. Experimental study on film cooling characteristics of lamilloy at different blowing ratios[J]. Thermal power generation, 2015, 44(9): 43-47.
DOI:
LI Guangchao, CAO Xifeng, LIU Yongquan, et al. Experimental study on film cooling characteristics of lamilloy at different blowing ratios[J]. Thermal power generation, 2015, 44(9): 43-47.DOI:
Experimental study on film cooling characteristics of lamilloy at different blowing ratios
The narrow-band transient liquid crystal technique was applied to carry out experimental investigation on cooling efficiency and heat transfer coefficient of the outer surface of a narrow chamber lamilloy with double-row film cooling holes
under conditions with blowing ratio of 1.0
1.5and 2.0
and film hole injection angle of 30°and 90°.The results show that
for the lamilloy model
the film cooling efficiency in downstream area of the double-row hole decreased with the increasing blowing ratio.The distribution of cooling efficiency is different for film holes with different injection angles.For lamilloys with injection angle of 30°and 90°
the surface heat transfer coefficient of the film hole changed little with the blowing ratio.
Orthogonal simulation of multi-factor influenced film cooling efficiency
Numerical simulation on cooling effectiveness of gas film on tip of blade with groove and fins
Investigation on film cooling effectiveness of fanned hole with broad outlet
Effects of attack angle and endwall slippage on flow and heat transfer of blade squealer tip
Related Author
ZHANG Ling
ZHU Jian
SHI Jingkai
WANG Chong
LI Guangchao
PENG Ningjian
ZHANG Wei
KOU Zhihai
Related Institution
Inner Mongolia Daihai Power Generation Co., Ltd
School of Energy and Power Engineering, Northeast Electric Power University
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 Measurement and Test Technology for Aviation Propulsion System,Faculty of Aerospace Engineering,Shenyang Aerospace University Shenyang
Liaoning Key Lab of Advanced Test and Measurement for Aviation Propulsion System,Shenyang Aerospace University