首页 | 本学科首页   官方微博 | 高级检索  
     检索      

弹用航空发动机尾喷流红外抑制技术研究
引用本文:翟普,隋俊友,崔杰,赵克云,孙华,徐祥春.弹用航空发动机尾喷流红外抑制技术研究[J].推进技术,1996,17(4):17-20,31.
作者姓名:翟普  隋俊友  崔杰  赵克云  孙华  徐祥春
作者单位:航天工业总公司31所,北京机电工程研究所
摘    要:详细介绍了弹用航空发动机红外抑制技术开展的一系列试验和数值分析。这些工作均取得了较好的结果,为今后此项技术的进一步深入研究直至工程应用打下了良好的基础。

关 键 词:航空发动机,喷管气流,红外特征,红外抑制

A RESEARCH ON RADIATION RESTRICTION TECHNIQUE OF A NOZZLE FLOW OF AERO-ENGINE FOR MISSILE
Zhai Pu, Sui Junyou, Cui Jie, Zhao Keyun.A RESEARCH ON RADIATION RESTRICTION TECHNIQUE OF A NOZZLE FLOW OF AERO-ENGINE FOR MISSILE[J].Journal of Propulsion Technology,1996,17(4):17-20,31.
Authors:Zhai Pu  Sui Junyou  Cui Jie  Zhao Keyun
Institution:Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074
Abstract:In this paper experiments and the numerical analyses about infrared restriction technique of aero-engine is described in detail. Satisfactory results are obtained, which lay a good functionfor the future research and application.
Keywords:Aircraft engine  Nozzle gas flow  Infrared signature  Infrared suppression
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号