首页|期刊导航|Advances in Aerodynamics|Numerical simulation of fluid-structure interaction for solid rocket engine nozzle ablation

Numerical simulation of fluid-structure interaction for solid rocket engine nozzle ablation

Donghui Wang Dehua Cao Zhitan Zhou Ranhui Liang

Advances in Aerodynamics2025，Vol.7Issue(1)：P.51-68,18.

Advances in Aerodynamics2025，Vol.7Issue(1)：P.51-68,18.DOI:10.1186/s42774-024-00192-2

Numerical simulation of fluid-structure interaction for solid rocket engine nozzle ablation

Donghui Wang ¹Dehua Cao ²Zhitan Zhou ³Ranhui Liang³

作者信息

1. National University of Defense Technology,Changsha 410073,People''s Republic of China
2. Nanchang Hangkong University,Nanchang 330063,People''s Republic of China Tianjin Aerospace Reliability Technology Co.,Ltd,Tianjin 300462,People''s Republic of China
3. Nanchang Hangkong University,Nanchang 330063,People''s Republic of China
折叠

摘要

关键词

Laval nozzle/Thermochemical ablation/C/C composite materials/Multiphysics coupling

分类

航空航天

引用本文复制引用

Donghui Wang,Dehua Cao,Zhitan Zhou,Ranhui Liang..Numerical simulation of fluid-structure interaction for solid rocket engine nozzle ablation[J].Advances in Aerodynamics,2025,7(1):P.51-68,18.

基金项目

financially supported by Jiangxi Provincial Natural Science Foundation(20224BAB211010,20232BAB201031)。（20224BAB211010,20232BAB201031）

Advances in Aerodynamics

ISSN：2097-3462

访问量0

下载量0

段落导航