期刊文献+

大压缩比两级燃气引射系统参数匹配试验研究 被引量:4

Experimental investigation on parameter matching of high compression-ratio two-stage gas ejector system
下载PDF
导出
摘要 建立了单模块两级超声速环形引射系统,采用不同参数的高温燃气分别作为一二级引射器驱动工质,对二级引射器单独启动特性、两级引射器自身参数匹配特性及有负载情况下系统匹配特性进行了试验研究。研究结果表明:二级引射器单独启动存在流量下限;两级引射器自身参数匹配范围是比较宽的,但在有负载情况下,其匹配范围大为缩小;对于多级引射而言,各级引射气体压力与负载压力的相互匹配至关重要。 A single-module two-stage ejector test facility was established to investigate the supersonic ejector performance. and hot gases with various were used as parameters first-stage and second-stage driving fluids. The investigation indicates that there is a lower limit of flux when second-stage ejector start alone, and the parameter matching range is relatively wide for the system itself, but the parameter matching range will reduce greatly for the system with load. Pressure matching is a all-important question for multi-stage ejector.
出处 《强激光与粒子束》 EI CAS CSCD 北大核心 2008年第10期1589-1592,共4页 High Power Laser and Particle Beams
基金 国家高技术发展计划项目
关键词 引射器 高真空 两级燃气引射系统 参数匹配 Ejector High vacuum Two-stage gas ejector Parameter matching
  • 相关文献

参考文献9

二级参考文献24

  • 1凌其扬,廖达雄,陶祖贤.风洞引射器试验研究[J].气动实验与测量控制,1994,8(2):10-18. 被引量:12
  • 2徐万武,邹建军,王振国,周进.超声速环型引射器启动特性试验研究[J].火箭推进,2005,31(6):7-11. 被引量:22
  • 3廖达雄,任泽斌,余永生,杨永.等压混合引射器设计与实验研究[J].强激光与粒子束,2006,18(5):728-732. 被引量:47
  • 4[1]Taylor,Delbert.Supersonic ejectors[R].GARD-AG-163.
  • 5[2]R C Bauer,R C German.The effect of second throat geometry on the performauce of ejectors without induced flow[R].AEDC-TN-61-133.
  • 6[3]James W Hale.Comparison of diffuser-ejector performance with five different driving fluids[R].AEDC-TDR-63- 207,1963.
  • 7Bauer R C, German R. The effect of secod throat geometry on the performance of ejectors without induced flow [ R ].AEDC-TN-61-133.
  • 8Jones W L, Friee H G and Lorenzo C F. Experimental study of zero-flow ejectors using gasous nitrogen[ R]. NASA TND-203.
  • 9Kazuyasu Matsuo, Yoshiaki Miyazato, Heuy-Dong Kim.Shock train and pseudo-shock phenomena in internal gas flows[J]. Progress in Aerospace Sciences. 1999, 35:33-100.
  • 10Emanuel G. Optimum performance for a single-stage gaseous ejector[J]. AIAA Journal ,1974, 14(9) : 1292-1296.

共引文献76

同被引文献42

引证文献4

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部