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

临近空间高超声速飞行器黑障问题研究综述
引用本文:龚旻,谭杰,李大伟,马召,田冠锁,王暕来,孟令涛.临近空间高超声速飞行器黑障问题研究综述[J].宇航学报,2018,39(10):1059-1070.
作者姓名:龚旻  谭杰  李大伟  马召  田冠锁  王暕来  孟令涛
作者单位:中国运载火箭技术研究院,北京 100076
基金项目:国防基础科研计划(JCKY2016203B115)
摘    要:首先对国内外黑障问题研究历史进行了回顾,然后从等离子体鞘套形成机理和基本特征、电波传播机理及信道特征等方面阐述了高超声速飞行器黑障问题的成因。随后,着重介绍了等离子体流场和电波传播数值模拟方法并分析了方法的适用性。进一步对等离子体地面模拟方法和诊断技术进行了概述,并对国内外地面黑障实验结果进行了详细分析。在此基础上,针对临近空间高超声速飞行器的特点,采用层次分析法(AHP)对现有黑障消除技术进行了评估,给出了目前工程实用方法、近期可能实现的工程实用解以及未来具有应用潜力的消除技术。最后,对黑障问题后续研究方向提出了几点建议。

关 键 词:临近空间高超声速飞行器  黑障  等离子体鞘套  电波传播  
收稿时间:2018-03-19

Review of Blackout Problems of Near Space Hypersonic Vehicles
GONG Min,TAN Jie,LI Da wei,MA Zhao,TIAN Guan suo,WANG Jian lai,MENG Ling tao.Review of Blackout Problems of Near Space Hypersonic Vehicles[J].Journal of Astronautics,2018,39(10):1059-1070.
Authors:GONG Min  TAN Jie  LI Da wei  MA Zhao  TIAN Guan suo  WANG Jian lai  MENG Ling tao
Institution:China Academy of Launch Vehicle Technology, Beijing 100076, China
Abstract:A brief review on the studies of blackout problems is given, and the causes of blackout are elucidated from the aspects of plasma sheath generation, electromagnetic wave transmission mechanism and channel characteristics. Secondly, the numerical simulation methods of plasma flows and radio wave propagation in plasma are emphatically introduced, and the adaptability analysis of these methods is carried out. Furthermore, the plasma reproducing technologies as well as plasma diagnostic techniques are summarized, and the ground experimental results of blackout are analyzed in detail. On the basis of that, blackout mitigating approaches are evaluated based on the analytical hierarchy process (AHP) method for near space hypersonic vehicles. The current practical approaches, near-term promising approaches and some potential solutions are proposed. Finally, some suggestions for further research direction of blackout problems are presented.
Keywords:   Near space hypersonic vehicles  Blackout  Plasma sheath  Radio wave propagation  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》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