Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor | |
Fan XJ(范学军); Yu G(俞刚); Li JG(李建国); Zhang XY(张新宇); Sung CJ | |
2004-07-11 | |
会议名称 | AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference |
卷号 | 22 |
期号 | 1 |
页码 | 103-110 |
通讯作者 | 范学军 |
中文摘要 | Injection and combustion of vaporized kerosene was experimentally investigated in a Mach 2.5 model combustor at various fuel temperatures and injection pressures. A unique kerosene heating and delivery system, which can prepare heated kerosene up to 820 K at a pressure of 5.5 MPa with negligible fuel coking, was developed. A three-species surrogate was employed to simulate the thermophysical properties of kerosene. The calculated thermophysical properties of surrogate provided insight into the fuel flow control in experiments. Kerosene jet structures at various preheat temperatures injecting into both quiescent environment and a Mach 2.5 crossflow were characterized. It was shown that the use ofvaporized kerosene injection holds the potential of enhancing fuel-air mixing and promoting overall burning. Supersonic combustion tests further confirmed the preceding conjecture by comparing the combustor performances of supercritical kerosene with those of liquid kerosene and effervescent atomization with hydrogen barbotage. Under the similar flow conditions and overall kerosene equivalence ratios, experimental results illustrated that the combustion efficiency of supercritical kerosene increased approximately 10-15% over that of liquid kerosene, which was comparable to that of effervescent atomization. |
收录类别 | CPCI-S |
会议录 | Journal of Propulsion and Power |
学科主题 | 力学 |
语种 | 英语 |
ISSN号 | 0748-4658 |
WOS记录号 | WOS:000234910900012 |
内容类型 | 会议论文 |
源URL | [http://dspace.imech.ac.cn/handle/311007/13857] |
专题 | 力学研究所_力学所知识产出(1956-2008) |
推荐引用方式 GB/T 7714 | Fan XJ,Yu G,Li JG,et al. Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor[C]. 见:AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference. |
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