Analysis of a Merged Shock-layer Based upon a Multi-temperature Model
Analysis of a Merged Shock-layer Based upon a Multi-temperature Model
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基于多温度模型的合并激波层分析
DOI：
10.11345/nctam.53.147
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发表时间：
2004
期刊：
影响因子：
--
通讯作者：
H. Shirai
中科院分区：
文献类型：
--
作者：
D. Watanabe;M. Funatsu;H. Shirai
当航天器以高超音速进入地球大气层时，在航天器上空形成强烈的弓形激波。如果进入速度超过10 km/s，激波后的温度变得如此之高，以至于激波层中的气体强烈辐射。众所周知，身体表面是
When a spacecraft enters the Earth’s atmosphere at a hypersonic velocity, a strong bow shock wave is formed over the spacecraft. If the entry velocity exceeds 10 km/s, the temperature behind the shock wave becomes so high that gas in the shock layer radiates strongly. It is well known that the body surface is