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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מידע ביבליוגרפי

Principais autores:	ZHOU Yunting, MA Changsheng, MA Jingwen, LE Guigao
פורמט:	Artigo
שפה:	Chinês
יצא לאור:	Editorial Office of Journal of Nanjing University of Aeronautics and Astronautics 2025-08-01
סדרה:	Nanjing Hangkong Hangtian Daxue Xuebao
נושאים:	launch vehicle new mobile launch pad thermal and mechanical loads gas jet drift
גישה מקוונת:	https://jnuaa.nuaa.edu.cn/njhkht/article/html/202504013?st=article_issue
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