Experiment was carried out to analyze the heat transfer characteristics of the inner surfaces of a kind of lamilloy configuration by using narrow-band transient liquid crystal technique.In this research
the ratio of hole pitch to impingement hole diameter(S/D) is 3.2
4.5
5.9
and Reynolds numbers range from 10 000 to 40 000.This paper also compared with traditional lamilloy model to analyze the heat transfer mechanism.The result shows that: heat transfer coefficient of the surfaces increases when Re becomes greater
and gradually decreases when the holes pitch becomes wider.The mathematics fit formulas of the Nu with respect to Re and S/D has also been given.
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Related Author
LIU Zhenxia
YANG Fu
LI Yanjun
宋远佳
赖欢
陈万华
高荣
张伟
Related Institution
中国空气动力研究与发展中心 设备设计及测试技术研究所
南京航空航天大学 航空宇航学院
China Aviation Power Machinery Research Institute, Aviation Industry Corporation of China
School of Power and Energy, Northwestern Polytechnical University,Xian
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics, School of Jet Propulsion, Beijing University of Aeronautics Astronautics