Preliminary Investigation of Full Model of Two-Mode Scramjet
文献类型：期刊论文
| 作者 | J.L. Le; Z.C. Zhang; H.C. Bai1; M.A. Goldfeld; R.V. Nestoulia; A.V. Starov2 |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2001 |
| 卷号 | 10期号:2页码:97,102 |
| 关键词 | Full Engine Hypersonic Flow Fuel Inlet Combustion Wind Tunnel Experiment. |
| 英文摘要 | In this paper results of previous researches of two-mode full engine model for Mach number range from3 to 6 are presented. The main aims of researches are to obtain characteristics of full engine model and its components (the inlet, the combustion chamber and the nozzle) in ramjet and scramjet regimes and to compare these characteristics with the calculation results according to CFD and to approximate (engineering) methods. Tests were carried out without fuel supply (cold tests) and with fuel supply (study of ignition and combustion).Hydrocarbon and hydrogen fuel (gaseous or liquid) were used during the tests |
| 公开日期 | 2013-03-12 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/53666]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | J.L. Le,Z.C. Zhang,H.C. Bai1,et al. Preliminary Investigation of Full Model of Two-Mode Scramjet[J]. JOURNAL OF THERMAL SCIENCE,2001,10(2):97,102. |
| APA | J.L. Le,Z.C. Zhang,H.C. Bai1,M.A. Goldfeld,R.V. Nestoulia,&A.V. Starov2.(2001).Preliminary Investigation of Full Model of Two-Mode Scramjet.JOURNAL OF THERMAL SCIENCE,10(2),97,102. |
| MLA | J.L. Le,et al."Preliminary Investigation of Full Model of Two-Mode Scramjet".JOURNAL OF THERMAL SCIENCE 10.2(2001):97,102. |
入库方式： OAI收割
来源：工程热物理研究所
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