Pulsed combustion of hydrocarbon fuels in a supersonic model combustor

	Pulsed combustion of hydrocarbon fuels in a supersonic model combustor
	Zhang TC(张泰昌); Fan XJ(范学军); Wang J(王晶); Li JG(李建国); Yu G(俞刚); Zhang TC(张泰昌)
会议录名称	47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
	2011
会议名称	47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
会议日期	JUL 31-AUG 03, 2011
会议地点	San Diego, CA, United states
摘要	Pulsed combustion of hydrocarbon fuels (ethylene and kerosene) in a Mach number 2.5 supersonic model combustor was experimentally investigated using a pulse spark igniter located in the center of a cavity. The results demonstrated that pure pulsed combustion of ethylene could exist at relatively low stagnant temperatures while pulse-induced stable combustion could be obtained at higher temperatures. Experiments also showed that no significant pulsed combustion of kerosene existed when ethylene was used as pilot flame because the combustion of pilot ethylene offers much more heat and radicals than that supplied by discharging of the spark plug. rights reserved.
课题组名称	LHD超声速燃烧
资助信息	American Institute for Aeronautics and Astronautics (AIAA)
ISBN号	9781600869495
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/48279
专题	高温气体动力学国家重点实验室
通讯作者	Zhang TC(张泰昌)
推荐引用方式 GB/T 7714	Zhang TC,Fan XJ,Wang J,et al. Pulsed combustion of hydrocarbon fuels in a supersonic model combustor[C]47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011,2011.

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