@inproceedings{a92d2da09777442a81d20a31f57db747,
title = "Temperature measurement at the exit of annular combustor with slinger in turbojet engine",
abstract = "This paper present the experimental results from a real turbojet engine with slinger annular combustor. The temperature of combustor outlet gas was measured with K-type thermocouples which were arranged in the guide turbine vanes. Both steady states and transition states were tested during the experiment. The experimental results of steady states indicated that the combustor outlet temperature distribution present reverse “C” shape which was lower at both ends and higher in the middle. The engine speed had greatly influence on combustor performance. Characteristics when engine working in transition states were also described.",
author = "Liu, \{Deng Huan\} and Jie Jin and Fang Wang and Song, \{Man Xiang\} and Pan, \{Nin Ming\} and Liu, \{Da Xiang\} and Jin, \{Wen Ming\}",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc, AIAA.; 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2015 ; Conference date: 22-06-2015 Through 26-06-2015",
year = "2015",
doi = "10.2514/6.2015-2560",
language = "英语",
isbn = "9781624103643",
series = "31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference",
}