Impact Characteristics of Rocket Engine with Inclined Nozzle on a New Launch Pad
To investigate the impact characteristics of a launch vehicle equipped with inclined nozzle engines on a new type of launch platform， a rocket gas jet model is established based on the three-dimensional compressible multi-component transport Navier-Stokes equations， the Realizable k‑ε two-equation t...
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| Autors principals: | , , , |
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| Format: | Artigo |
| Idioma: | Chinês |
| Publicat: |
Editorial Office of Journal of Nanjing University of Aeronautics and Astronautics
2025-08-01
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| Col·lecció: | Nanjing Hangkong Hangtian Daxue Xuebao |
| Matèries: | |
| Accés en línia: | https://jnuaa.nuaa.edu.cn/njhkht/article/html/202504013?st=article_issue |
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