Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles
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Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles
Vol. 24, Issue 5, (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
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LI Guang-chao, ZHU Hui-ren, FAN Hui-ming. Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles[J]. 2009, 24(5).
DOI:
LI Guang-chao, ZHU Hui-ren, FAN Hui-ming. Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles[J]. 2009, 24(5).DOI:
Experimental investigation on film cooling of expanded hole at both inlet and outlet with various injection angles
To study the film cooling characteristics of expanded holes
heat transfer coefficient ratios and film cooling effectiveness was investigated downstream of a row of holes with inclination angles of 20° 45° and 90° as well as three varying hole diameters.Momentum flux ratios vary in the range of 1 to 4.The discussion was focused on the effect of momentum flux ratios and inclination angles on heat transfer coefficient ratios and film cooling effectiveness in the presence of mainstream zero pressure gradient.The experimental results show that the increasing momentum flux ratios leads to the increasing heat transfer coefficient ratios and film cooling effectiveness.The effect of momentum flux ratios on cooling effectiveness becomes weaker with the increase of angles.The angles have complex influence on heat transfer coefficient ratios.The increasing angles lead to the decreased cooling effectiveness.Film cooling effectiveness of inclination angle of 20° is bigger than those of 45° and 90°.
Numerical simulation of film cooling effectiveness with one inlet and double outlet hole on leading edge
Experimental investigation of rotating single-hole film cooling performance on suction side of a turbine blade
Numerical investigation on film cooling effectiveness at suction surface of stator blade
Numerical simulation of cooling effectiveness with injection of double-outlet hole
Film cooling experiment of row of expanded shape holes
Related Author
LI Guang-chao
ZHANG Wei
WANG Cheng-jun
PENG Da-wei
WANG Jian-ming
XU Zhi-hui
LI Guo-qing
DENG Hong-wu
Related Institution
Liaoning Key Laboratory of Digital Technology Simulation and Test Technique, School of Aero Dynamics and Energy Engineering, Shenyang Aerospace University
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Aircraft Design and Research Institute,Hongdu Aviation Industry Group
China Gas Turbine Establishment, Aviation Industry Corporation of China