Development of the facility for model scramjet testing
文献类型：会议论文
| 作者 | Chang XY(张新宇); Chen LH(陈立红) ; Yu G(俞刚); Qian DX(钱大兴)
|
| 出版日期 | 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 |
| 关键词 | Chinese Academy of Sciences Enthalpy flow Hypersonic propulsion test facility Performance tests Scramjet testing Supersonic combustion Total pressure Total temperatures |
| 中文摘要 | 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. |
| 收录类别 | EI |
| 会议网址 | http://dx.doi.org/10.4271/2001-01-4051 |
| 会议录 | 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference
 |
| 语种 | 英语 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60248]  |
| 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 | Chang XY,Chen LH,Yu G,et al. Development of the facility for model scramjet testing[C]. 见:10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001. Kyoto, Japan. April 24, 2001 - April 27, 2001.http://dx.doi.org/10.4271/2001-01-4051. |
入库方式： OAI收割
来源：力学研究所
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