Experimental study on combustion characteristics of Chinese RP-3 kerosene

IMR OpenIR

	Experimental study on combustion characteristics of Chinese RP-3 kerosene
其他题名	Experimental study on combustion characteristics of Chinese RP-3 kerosene
	Ma Hongan 1; Xie Maozhao 1; Zeng Wen 2; Chen Baodong 2
	2016
发表期刊	CHINESE JOURNAL OF AERONAUTICS
ISSN	1000-9361
卷号	29 期号:2 页码:375-385
摘要	In order to illustrate the combustion characteristics of RP-3 kerosene which is widely used in Chinese aero-engines, the combustion characteristics of RP-3 kerosene were experimentally investigated in a constant volume combustion chamber. The experiments were performed at four different pressures of 0.1 MPa, 0.3 MPa, 0.5 MPa and 0.7 MPa, and three different temperatures of 390 K, 420 K and 450 K, and over the equivalence ratio range of 0.6-1.6. Furthermore, the laminar combustion speeds of a surrogate fuel for RP-3 kerosene were simulated under certain conditions. The results show that increasing the initial temperature or decreasing the initial pressure causes an increase in the laminar combustion speed of RP-3 kerosene. With the equivalence ratio increasing from 0.6 to 1.6, the laminar combustion speed increases initially and then decreases gradually. The highest laminar combustion speed is measured under fuel rich condition (the equivalence ratio is 1.2). At the same time, the Markstein length shows the same changing trend as the laminar combustion speed with modification of the initial pressure. Increasing the initial pressure will increase the instability of the flame front, which is established by decreased Markstein length. However, different from the effects of the initial temperature and equivalence ratio on the laminar combustion speed, increasing the equivalence ratio will lead to a decrease in the Markstein length and the stability of the flame front, and the effect of the initial temperature on the Markstein length is unclear. Furthermore, the simulated laminar combustion speeds of the surrogate fuel agree with the corresponding experimental datas of RP-3 kerosene within similar to 10% deviation under certain conditions. (C) 2016 Chinese Society of Aeronautics and Astronautics. Published by Elsevier Ltd.
其他摘要	In order to illustrate the combustion characteristics of RP-3 kerosene which is widely used in Chinese aero-engines, the combustion characteristics of RP-3 kerosene were experimentally investigated in a constant volume combustion chamber. The experiments were performed at four different pressures of 0.1 MPa, 0.3 MPa, 0.5 MPa and 0.7 MPa, and three different temperatures of 390 K, 420 K and 450 K, and over the equivalence ratio range of 0.6-1.6. Furthermore, the laminar combustion speeds of a surrogate fuel for RP-3 kerosene were simulated under certain conditions. The results show that increasing the initial temperature or decreasing the initial pressure causes an increase in the laminar combustion speed of RP-3 kerosene. With the equivalence ratio increasing from 0.6 to 1.6, the laminar combustion speed increases initially and then decreases gradually. The highest laminar combustion speed is measured under fuel rich condition (the equivalence ratio is 1.2). At the same time, the Markstein length shows the same changing trend as the laminar combustion speed with modification of the initial pressure. Increasing the initial pressure will increase the instability of the flame front, which is established by decreased Markstein length. However, different from the effects of the initial temperature and equivalence ratio on the laminar combustion speed, increasing the equivalence ratio will lead to a decrease in the Markstein length and the stability of the flame front, and the effect of the initial temperature on the Markstein length is unclear. Furthermore, the simulated laminar combustion speeds of the surrogate fuel agree with the corresponding experimental datas of RP-3 kerosene within 10% deviation under certain conditions.
关键词	LAMINAR BURNING VELOCITY AIR MIXTURES MARKSTEIN LENGTHS SPHERICAL FLAMES INSTABILITIES PRESSURES NUMBER Combustion mechanism Combustion stability Laminar combustion speed Markstein length RP-3 kerosene
收录类别	CSCD
语种	英语
资助项目	[National Natural Science Foundation of China]
CSCD记录号	CSCD:5695765
引用统计	被引频次：9[CSCD] [CSCD记录]
文献类型	期刊论文
条目标识符	http://ir.imr.ac.cn/handle/321006/147258
专题	中国科学院金属研究所
作者单位	1.大连大学 2.中国科学院金属研究所
推荐引用方式 GB/T 7714	Ma Hongan,Xie Maozhao,Zeng Wen,et al. Experimental study on combustion characteristics of Chinese RP-3 kerosene[J]. CHINESE JOURNAL OF AERONAUTICS,2016,29(2):375-385.
APA	Ma Hongan,Xie Maozhao,Zeng Wen,&Chen Baodong.(2016).Experimental study on combustion characteristics of Chinese RP-3 kerosene.CHINESE JOURNAL OF AERONAUTICS,29(2),375-385.
MLA	Ma Hongan,et al."Experimental study on combustion characteristics of Chinese RP-3 kerosene".CHINESE JOURNAL OF AERONAUTICS 29.2(2016):375-385.