Hypersonic boundary layer when flying in the atmosphere of Mars

Research output: Contribution to journal › Article › peer-review

Translated title of the contribution	Гиперзвуковой пограничный слой при полете в атмосфере Марса
Original language	English
Pages (from-to)	5-24
Number of pages	20
Journal	Journal of Computational Technologies
Volume	29
Issue number	3
DOIs	https://doi.org/10.25743/ICT.2024.29.3.002
Publication status	Published - 2024

atmosphere of Mars, dissociation, finite difference scheme, hypersonic boundary layer, locally self-similar solutions, numerical calculations

ID: 60462773