IMECH-IR  > 高温气体动力学国家重点实验室
远程超低巡航飞行分析
樊菁
Source Publication第四届高超声速科技学术会议会议日程及摘要集
2011
Pages28
Conference Name第四届高超声速科技学术会议
Conference Date2011
Conference Place中国海南三亚
Abstract<正>提出一种新的巡航飞行方式,在地球表面的垂直方向上,利用离心力,辅之火箭推力,平衡重力,保持飞行高度;在地球表面的平行方向上,则依靠助推段获得的速度,惯性前进。这种飞行方式适合于高空稀薄气体环境,将巡航
Keyword高空 稀薄大气 超低巡航飞行 离心力 火箭推力
DepartmentLHD微尺度和非平衡流动
Funding Organization中国力学学会、中国科学院高超声速科技中心、中国科学院力学研究所、高温气体动力学国家重点实验室
URL查看原文
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/45283
Collection高温气体动力学国家重点实验室
Corresponding Author樊菁
Recommended Citation
GB/T 7714
樊菁. 远程超低巡航飞行分析[C],2011:28.
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