Experimental investigation of cavity-based scramjet model
文献类型：会议论文
| 作者 | Gu HB(顾洪斌) ; Chen LH(陈立红); 张新宇(Chang XY)
|
| 出版日期 | 2006 |
| 会议名称 | 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference |
| 会议日期 | November 6, 2006 - November 9, 2006 |
| 会议地点 | Canberra, Australia |
| 关键词 | Kerosene fuel Mass flow rate Scramjet engine |
| 中文摘要 | The configuration of scramjet engine is important to organize combustion with the kerosene fuel. Cavities and Struts are usually used to enhance mixing and hold flame. The present work focused on the performance of the model engine with the different inlets and combustors. The models were tested in a free-jet wind tunnel that typically provides the testing flow with Mach number of 5.8, total temperature of 1800K, and total pressure of 4.5MPa and mass flow rate of 4kg/s. Strut as effective techniques were used in a kerosene-fueled scramjet. The integration of strut/cavities also had the important effect to make the combustion more stable than the model without strut. The one dimensional analysis method has been used to analyze the main characteristics of the models. |
| 收录类别 | EI |
| 会议录 | A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference
 |
| 语种 | 英语 |
| ISBN号 | 1563478269 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60290]  |
| 专题 | 力学研究所_力学所知识产出(1956-2008) |
| 推荐引用方式 GB/T 7714 | Gu HB,Chen LH,Zhang XY. Experimental investigation of cavity-based scramjet model[C]. 见:14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference. Canberra, Australia. November 6, 2006 - November 9, 2006. |
入库方式： OAI收割
来源：力学研究所
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