Effect of gas blowing on the head of thermal ablation vehicle
Abstract The reentry vehicle will encounter thermal ablation, especially at the stagnation point regime. A theoretical work has been done to analyze the thermal effect of gas blowing due to thermal ablation of surface material on the head of a general hypersonic vehicle. By deriving the formulation,...
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| Autores principales: | , , , |
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| Formato: | Artigo |
| Lenguaje: | Inglês |
| Publicado: |
SpringerOpen
2022-03-01
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| Colección: | Advances in Aerodynamics |
| Materias: | |
| Acceso en línea: | https://doi.org/10.1186/s42774-021-00097-4 |
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