IMECH-IR  > 高温气体动力学国家重点实验室
高超声速高温气体效应判据
Alternative TitleCRITERIA ON HIGH-TEMPERATURE GAS EFFECTS AROUND HYPERSONIC VEHICLES
樊菁
Source Publication力学学报
2010-07-18
Volume42Issue:4Pages:591-596
Abstract基于动理论的观点,提出几种定量判据,用以判断在怎样的飞行条件下,高超声速飞行器周围高温空气分子的振动、离解、电离效应是重要的.
Keyword高超声速飞行 高温气体效应 分子振动 离解 电离
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Indexed ByEI ; CSCD
Language中文
Funding Organization国家自然科学基金创新群体项目(10621202)资助~~
CSCD IDCSCD:3903539
Citation statistics
Cited Times:6[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43864
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. 高超声速高温气体效应判据[J]. 力学学报,2010,42(4):591-596.
APA 樊菁.(2010).高超声速高温气体效应判据.力学学报,42(4),591-596.
MLA 樊菁."高超声速高温气体效应判据".力学学报 42.4(2010):591-596.
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