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Heating of Two-Layer Thermal Protection Coating at Hypersonic Flow around a Spherical Blunting
Russian Aeronautics Pub Date : 2021-05-26 , DOI: 10.3103/s1068799821010116
V. S. Zarubin , V. N. Zimin , V. V. Leonov , V. S. Zarubin

Abstract

The nonstationary problem of thermal conductivity in a two-layer thermal protection coating is under consideration. The solution is given for a metal hemispherical shell with axisymmetrical distribution of the heat flux density over the outer surface of the coating.



中文翻译:

球形钝头周围高超声速流动下的两层热保护涂层的加热

摘要

正在考虑两层热保护涂层中的热导率的非平稳问题。针对金属半球形壳给出了解决方案,该半球形壳的热通量密度在涂层的外表面上呈轴对称分布。

更新日期:2021-05-26
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