| 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)
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| Source Publication | 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 |
| 2011 | |
| Conference Name | 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 |
| Conference Date | JUL 31-AUG 03, 2011 |
| Conference Place | San Diego, CA, United states |
| Abstract | 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. |
| Department | LHD超声速燃烧 |
| Funding Organization | American Institute for Aeronautics and Astronautics (AIAA) |
| ISBN | 9781600869495 |
| Indexed By | EI |
| Language | 英语 |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/48279 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Zhang TC(张泰昌) |
| Recommended Citation 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. |
| Files in This Item: | ||||||
| File Name/Size | DocType | Version | Access | License | ||
| 6.2011-5547.pdf（399KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Application Full Text | ||
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