Experimental investigation on the cavity-based scramjet model
文献类型：期刊论文
| 作者 | Gu HB(顾洪斌) ; Chen LH(陈立红); Zhang XY(张新宇); Gu HB(顾洪斌)
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| 刊名 | CHINESE SCIENCE BULLETIN
 |
| 出版日期 | 2009 |
| 卷号 | 54期号:16页码:2794-2799 |
| 通讯作者邮箱 | guhb@imech.ac.cn |
| 关键词 | scramjet combustor cavity performance |
| ISSN号 | 1001-6538 |
| 通讯作者 | 顾洪斌 |
| 合作状况 | 其它 |
| 中文摘要 | The present work focused on improving the engine performance with different fuel equivalence ratios and fuel injections. A scramjet model with strut/cavity integrated configurations was tested under Mach 5.8 flows. The results showed that the strut may sreve as an effective tool in a kerosene-fueled scramjet. The integration of strut/cavities also had great effect on stablizing the combustion in a wide range of fuel equivalence ratio. The one-sdimensional analysis method was used to analyze the main characteristics of the model. The two-stage fuel injection should have better performance in increasing the chemical reaction rate in the first cavity region. |
| 学科主题 | 弹性力学与塑性力学 |
| 类目[WOS] | Science & Technology - Other Topics |
| 关键词[WOS] | SUPERSONIC COMBUSTORS; FUEL-INJECTION; FLAME STABILIZATION; PERFORMANCE; FLOW; MECHANISM |
| 收录类别 | SCI |
| 语种 | 英语 |
| WOS记录号 | WOS:000269212800010 |
| 公开日期 | 2009-09-28 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/26508]  |
| 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 | Gu HB(顾洪斌) |
| 推荐引用方式 GB/T 7714 | Gu HB,Chen LH,Zhang XY,et al. Experimental investigation on the cavity-based scramjet model[J]. CHINESE SCIENCE BULLETIN,2009,54(16):2794-2799. |
| APA | Gu HB,Chen LH,Zhang XY,&顾洪斌.(2009).Experimental investigation on the cavity-based scramjet model.CHINESE SCIENCE BULLETIN,54(16),2794-2799. |
| MLA | Gu HB,et al."Experimental investigation on the cavity-based scramjet model".CHINESE SCIENCE BULLETIN 54.16(2009):2794-2799. |
入库方式： OAI收割
来源：力学研究所
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