Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
文献类型：期刊论文
| 作者 | Yao, Wei1,2 ; Liu, Hang1,2; Xue, Lianjie1,2; Xiao, Yabing1,2; Yao W(姚卫); Xiao YB(肖雅彬); Yue LJ(岳连捷); Yue LJ(岳连捷); Xiao YB(肖雅彬); Yao W(姚卫)
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| 刊名 | AEROSPACE SCIENCE AND TECHNOLOGY
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| 出版日期 | 2021-10-01 |
| 卷号 | 117页码:14 |
| 关键词 | Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| ISSN号 | 1270-9638 |
| DOI | 10.1016/j.ast.2021.106941 |
| 通讯作者 | Yao, Wei(weiyao@imech.ac.cn) |
| 英文摘要 | The uninstalled performance of a full-scale scramjet operating over Mach 7 to 10 and altitudes of 28 to 40 km was numerically analyzed by using high-fidelity Improved Delayed Detached Eddy Simulation (IDDES) with 125.10 million cells and Dynamic Zone Flamelet model (DZFM) with 21,294 flamelet zones. The inviscid thrust can be well correlated with dynamic pressure in the form of a gaussian function, whereas the viscous drag increases almost linearly with dynamic pressure. For the examined scramjet, net thrust is achieved for the low dynamic pressure range below 37 kPa and the high range above 55 kPa. The rule of mixed is burnt is observed, and the final combustion efficiencies vary from 66% to 82%. The upstream propagation of combustion occurs for most of the cases in the current strut-based combustor, and unstart occurs for the case of Mach 7 at 30 km. (C) 2021 Elsevier Masson SAS. All rights reserved. |
| WOS关键词 | LARGE-EDDY SIMULATION ; CONDITIONAL MOMENT CLOSURE ; DISSIPATION RATE ; JET ; COMBUSTION ; INJECTION ; DIFFUSION ; FLAMES ; LES |
| 资助项目 | National Key Research and Development Program of China[2019YFB1704202] ; Strategic Priority Research Program of Chinese Academy of Sciences[XDA17030X00] ; Training Program of the Major Research Plan of the National Natural Science Foundation of China[91641110] |
| WOS研究方向 | Engineering |
| 语种 | 英语 |
| WOS记录号 | WOS:000705191600007 |
| 资助机构 | National Key Research and Development Program of China ; Strategic Priority Research Program of Chinese Academy of Sciences ; Training Program of the Major Research Plan of the National Natural Science Foundation of China |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/87590]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 通讯作者 | Yao, Wei |
| 作者单位 | 1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China 2.Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China |
| 推荐引用方式 GB/T 7714 | Yao, Wei,Liu, Hang,Xue, Lianjie,et al. Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2021,117:14. |
| APA | Yao, Wei.,Liu, Hang.,Xue, Lianjie.,Xiao, Yabing.,姚卫.,...&Yao W.(2021).Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling.AEROSPACE SCIENCE AND TECHNOLOGY,117,14. |
| MLA | Yao, Wei,et al."Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling".AEROSPACE SCIENCE AND TECHNOLOGY 117(2021):14. |
入库方式： OAI收割
来源：力学研究所
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