Experimental investigation of cavity-based scramjet model

IMECH-IR > 力学所知识产出(1956-2008)

	Experimental investigation of cavity-based scramjet model
	Gu HB(顾洪斌); Chen LH(陈立红); 张新宇(Chang XY)
会议录名称	A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference
	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
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.
关键词	Kerosene Fuel Mass Flow Rate Scramjet Engine
ISBN号	1563478269
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/60290
专题	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]A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference,2006.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
CaEi053.pdf（162KB）	会议论文		开放获取	CC BY-NC-SA	浏览下载