Prediction of Hypersonic Boundary Layer Transition on Ablative Rough Surfaces of Deep Space Reentry Capsules

Prediction of Hypersonic Boundary Layer Transition on Ablative Rough Surfaces of Deep Space Reentry Capsules

In order to improve aerodynamic deceleration efficiency, deep space reentry capsules generally adopt large blunt windward shape and ablative heat protection system. However, factors such as the flat forebody shape and the sharp increase in surface roughness caused by aerothermodynamic heating and ab...

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Bibliographic Details
Main Authors: Qi LI, Rui ZHAO, Zhi CHEN, Bin GUO, Qiang WANG
Format: Article
Language:zho
Published: China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases 2024-01-01
Series:气体物理
Subjects:
deep space reentry capsule
large blunt heat shield
distributed rough element
transition mode
chemical non-equilibrium
Online Access:http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1073

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http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1073

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