Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions
文献类型：期刊论文
| 作者 | Zhong FQ(仲峰泉) ; Fan XJ(范学军); Yu G(俞刚); Li JG(李建国); Sung CJ
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| 刊名 | Journal of Thermophysics and Heat Transfer
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| 出版日期 | 2011 |
| 卷号 | 25期号:3页码:450-456 |
| 通讯作者邮箱 | fzhong@imech.ac.cn |
| 关键词 | Tetralin Decalin |
| ISSN号 | 0887-8722 |
| 产权排序 | [Zhong, Fengquan; Fan, Xuejun; Yu, Gong; Li, Jianguo] Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China; [Sung, Chih-Jen] Univ Connecticut, Dept Mech Engn, Storrs, CT 06269 USA |
| 通讯作者 | Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China |
| 合作状况 | 国际 |
| 中文摘要 | Thermal cracking and endothermicity of China No. 3 aviation kerosene were studied experimentally under supercritical conditions relevant to regenerative cooling systems for scramjet applications. A multiple-stage heating system with reaction products collection was used that can achieve a fuel temperature range of 780-1050 K, a pressure range of 3-4.5 MPa, and a residence time range of 0.6-3 s. The chemical heat sink was determined through a control volume analysis of the fuel flow. Compositions of I he cracked gaseous and liquid products were analyzed via gas chromatography. Based on the results of fuel conversion, the temperature range for the active cracking was observed to be approximately 800-1000 K, beyond which the cracking approaches completion. It was also found that the variation of the chemical heat sink with temperature can be nonmonotonic and a maximum endothermicity was seen to occur in the temperature range of 900-960 K, depending on the residence time. For the current operation conditions, the maximum chemical heat sink reached 0.5 MJ/k g at a fuel conversion of 45%. Composition analysis of the gaseous product indicated that the saturated hydrocarbons such as methane became dominant as temperature was increased. On the other hand, the major compositions of the liquid product were benzene-based and naphthalene-based hydrocarbons. |
| 学科主题 | Thermodynamics; Engineering |
| 分类号 | Q3 |
| 类目[WOS] | Thermodynamics ; Engineering, Mechanical |
| 研究领域[WOS] | Thermodynamics ; Engineering |
| 关键词[WOS] | TETRALIN ; DECALIN |
| 收录类别 | SCI ; EI |
| 原文出处 | http://www1.aiaa.org/content.cfm?pageid=406&gTable=jaPaper&gid=51399 |
| 语种 | 英语 |
| WOS记录号 | WOS:000293259600015 |
| 公开日期 | 2012-04-01 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/45173]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 推荐引用方式 GB/T 7714 | Zhong FQ,Fan XJ,Yu G,et al. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions[J]. Journal of Thermophysics and Heat Transfer,2011,25(3):450-456. |
| APA | 仲峰泉,范学军,俞刚,李建国,&Sung CJ.(2011).Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions.Journal of Thermophysics and Heat Transfer,25(3),450-456. |
| MLA | 仲峰泉,et al."Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions".Journal of Thermophysics and Heat Transfer 25.3(2011):450-456. |
入库方式： OAI收割
来源：力学研究所
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