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On the Transient Numerical Simulation of Solid Rocket Motor by Coupling Quasi One-Dimension Internal Flow with Three- Dimension Propellant Grain Burnback

Juan Duan Yongliang Xiong Ningdong Hu

哈尔滨工业大学学报（英文版）2021，Vol.28Issue(5)：15-27,13.

On the Transient Numerical Simulation of Solid Rocket Motor by Coupling Quasi One-Dimension Internal Flow with Three- Dimension Propellant Grain Burnback

Juan Duan ¹Yongliang Xiong ²Ningdong Hu¹

作者信息

1. Department of Mechanics,Huazhong University of Science and Technology,Wuhan 430074,China
2. Hubei Key Laboratory of Engineering Structural Analysis and Safety Assessment,Wuhan 430074,China
折叠

摘要

关键词

transient compressible solver/internal ballistics simulation/level-set method/solid rocket motor

Key words

transient compressible solver/internal ballistics simulation/level-set method/solid rocket motor

分类

航空航天

引用本文复制引用

Juan Duan,Yongliang Xiong,Ningdong Hu..On the Transient Numerical Simulation of Solid Rocket Motor by Coupling Quasi One-Dimension Internal Flow with Three- Dimension Propellant Grain Burnback[J].哈尔滨工业大学学报（英文版）,2021,28(5):15-27,13.

基金项目

Sponsored by the National Natural Science Foundation of China(Grant Nos.11872187 and 51779097)and the National Natural Science Foundation of Hubei Province(Grant No.2018CFB461). （Grant Nos.11872187 and 51779097）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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