Experimental research on film cooling characteristics of cylindrical hole with transient liquid crystal measurement technique
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Experimental research on film cooling characteristics of cylindrical hole with transient liquid crystal measurement technique
Vol. 24, Issue 9, (2009)
作者机构:
西北工业大学动力与能源学院,西安,710072
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
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LIU Cun-liang, ZHU Hui-ren, BAI Jiang-tao, et al. Experimental research on film cooling characteristics of cylindrical hole with transient liquid crystal measurement technique[J]. 2009, 24(9).
DOI:
LIU Cun-liang, ZHU Hui-ren, BAI Jiang-tao, et al. Experimental research on film cooling characteristics of cylindrical hole with transient liquid crystal measurement technique[J]. 2009, 24(9).DOI:
Experimental research on film cooling characteristics of cylindrical hole with transient liquid crystal measurement technique
Film cooling characteristics of cylindrical hole were measured using a transient liquid crystal measurement technique which can process nonuniform initial temperature.The influence of momentum flux ratio was tested.The results show that jets of large momentum ratio lift off from the wall after ejecting out and the cooling effectiveness in the upstream is very low.However
the area covered by jet and the effectiveness increase streamwise because the jets reattach the wall after lifting off
and moreover the cooling effectiveness in the region between adjacent holes is higher than that in the downstream hole centerline region.The cooling effectiveness distribution of small momentum ratio is just opposite to that of large momentum ratio.The normalized heat transfer coefficient distributions are similar for all momentum ratios in the downstream region.Heat transfer in the region between jets is stronger than the heat transfer in the hole centerline region because of the couple vortices.In the upstream region
a large and strong vortex is induced by the lifting off jet.And
a local region with high normalized heat transfer coefficient is formed due to this vortex.
Effect of trench hole depth and momentum flux ratio on film cooling characteristics
Experimental investigation on effect of small auxiliary holes on film cooling effectiveness
Experimental research on film cooling characteristics of cylindrical hole and expanding hole on the leading edge
Study on the physics of film-cooling effectiveness enhancement by the converging-expanding hole
Influence of aerodynamic parameters on film cooling effectiveness on the vane leading edge
Related Author
WANG Zhen-wei
ZHU Hui-ren
ZHANG Zong-wei
MENG Qing-kun
LIU Xiao-hong
TAO Zhi
LUO Xiang
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Related Institution
School of Engine and Energy, Northwestern Polytechnical University
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Department of Thermal Science and Energy Engineering,University of Science and Technology of China
Shenyang Engine Research Institute,Aero Engine Corporation of China
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics