Analysis of Aerodynamic Heating Modes in Thermochemical Nonequilibrium Flow for Hypersonic Reentry

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Analysis of Aerodynamic Heating Modes in Thermochemical Nonequilibrium Flow for Hypersonic Reentry

Thermochemical nonequilibrium significantly affects the accurate simulation of the aerothermal environment surrounding a hypersonic reentry vehicle entering Earth’s atmosphere during deep space exploration missions. The different heat transfer modes corresponding to each internal energy mode and che...

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Bibliographic Details
Main Authors:	Shuai He, Wei Zhao, Xinyue Dong, Zhuzhu Zhang, Jingying Wang, Xinglian Yang, Shiyue Zhang, Jiaao Hao, Ke Sun
Format:	Article
Language:	English
Published:	MDPI AG 2025-06-01
Series:	Energies
Subjects:	hypersonic reentry numerical simulation thermochemical nonequilibrium aerodynamic heating deep space exploration
Online Access:	https://www.mdpi.com/1996-1073/18/13/3417
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