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樊菁. 高超声速高温气体效应判据[J]. 力学学报, 2010, 42(4): 591-596. DOI: 10.6052/0459-1879-2010-4-lxxb2010-088
引用本文: 樊菁. 高超声速高温气体效应判据[J]. 力学学报, 2010, 42(4): 591-596. DOI: 10.6052/0459-1879-2010-4-lxxb2010-088
Criteria on high-temperature gas effects around hypersonic vehicles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(4): 591-596. DOI: 10.6052/0459-1879-2010-4-lxxb2010-088
Citation: Criteria on high-temperature gas effects around hypersonic vehicles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(4): 591-596. DOI: 10.6052/0459-1879-2010-4-lxxb2010-088

高超声速高温气体效应判据

Criteria on high-temperature gas effects around hypersonic vehicles

  • 摘要: 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.

     

    Abstract: Based on the kinetic viewpoint, several quantitative criteria are suggested to measure at which flight conditions the molecular vibration, dissociation and ionization of high-temperature air around hypersonic vehicles become important.Key words hypersonic flight, high-temperature effects, molecular vibration, dissociation, ionization

     

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