Development of the facility for model scramjet testing

IMECH-IR > 力学所知识产出(1956-2008)

	Development of the facility for model scramjet testing
	Chang XY(张新宇); Chen LH(陈立红); Yu G(俞刚); Qian DX(钱大兴)
会议录名称	10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference
	2001
会议名称	10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001
会议日期	April 24, 2001 - April 27, 2001
会议地点	Kyoto, Japan
摘要	A hypersonic propulsion test facility has been constructed in IMCAS (Institute of Mechanics, Chinese Academy of Sciences) in order to provide a high enthalpy hypersonic flow for a model scramjet testing. The vitiated air is produced by a hydrogen/air and oxygen replenishment combustion heater with flow rate of 3.5kg/s, total pressure of 5MPa and total temperature of 2000K in maximum, and accelerated up to Mach 5.6 by a two-dimensional nozzle. Test chamber of the facility is evacuated by a one-stage central air ejector. The preliminary facility performance tests showed that the vitiated air heater could provide the high enthalpy flow as expected. A copper model scramjet without cooling is ready for testing. © 2001 The American Institute of Aeronautics and Astronautics Inc. All rights reserved.
关键词	Chinese Academy Of Sciences Enthalpy Flow Hypersonic Propulsion Test Facility Performance Tests Scramjet Testing Supersonic Combustion Total Pressure Total Temperatures
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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/311007/60248
专题	力学所知识产出(1956-2008)
推荐引用方式 GB/T 7714	Chang XY,Chen LH,Yu G,et al. Development of the facility for model scramjet testing[C]10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference,2001.

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