@inproceedings{79ffabf33a7d4d57adfba731b0c82688,
title = "Effect of second-stage configuration on combustion in a dual-struts based staged supersonic combustor",
abstract = "A two staged supersonic combustor with one strut at each stage was utilized to investigate the effect of the downstream strut configuration on the combustion efficiency. Two configurations were experimentally investigated in a direct-connected facility with a vitiated heater providing Mach 2.0 air-flow with total temperature of 1231K. The results showed that when downstream strut injected separetely at high equivalence ratio, the configuration with a wedge at the trailing edge obtained more combustion efficiency than the one without. When the fuel injected from two struts together, the influnce of configuration on combustion efficiency was affected by the equivalence ratio distribution and the injection position on the two struts.",
author = "Liang Tian and Shaohua Zhu and Zheng Qin and Xuan Li and Xu Xu",
note = "Publisher Copyright: {\textcopyright} 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 ; Conference date: 28-07-2014 Through 30-07-2014",
year = "2014",
doi = "10.2514/6.2014-3780",
language = "英语",
series = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
}