@inproceedings{f816cbd7bcfb4f79997da4b49eead392,
title = "Research on aerodynamic characteristics of air-cooled turbine blade with conjugate heat transfer method",
abstract = "In order to improve the performance of aero engines, trying to increase the turbine inlet temperature is an important way. But the turbine inlet temperature of modern aero engines can be more than 2000 K, which is far more than what the materials can bear. So advanced cooling technologies should be introduced to solve this problem. Using the conjugate heat transfer method, this paper researched the aerodynamic characteristics of a certain turbine blade with complex cooling structures. Some conclusions can be drawn: the velocity of the air flow and different distributions of coolant flow for turbine blade with multiple cooling air inlets have great influence on the cooling effect; the cooling effect decreases as the temperature ratio decreases; with the same mass cold gas, the less film cooling holes, the worse cooling effect; therefore, a reasonable air flow distribution plays an important role in obtaining good cooling effect.",
keywords = "Air-cooled turbine, Conjugate heat transfer, Cooling effect",
author = "Zhang, \{Jing Jing\} and Wang, \{Lian Fu\} and Fang, \{Xiang Jun\}",
year = "2013",
doi = "10.4028/www.scientific.net/AMR.732-733.270",
language = "英语",
isbn = "9783037857434",
series = "Advanced Materials Research",
publisher = "Trans Tech Publications Ltd",
pages = "270--275",
booktitle = "Thermal, Power and Electrical Engineering",
address = "瑞士",
note = "2013 2nd International Conference on Energy and Environmental Protection, ICEEP 2013 ; Conference date: 19-04-2013 Through 21-04-2013",
}