首页|期刊导航|中国航空学报（英文版）|Pressure oscillation and suppression method of large-aspect-ratio solid rocket motors

Pressure oscillation and suppression method of large-aspect-ratio solid rocket motors

Yunzhi XI Jingwei GAO Zeping WU Bolun ZHANG Lijun YANG Jun XIA

中国航空学报（英文版）2025，Vol.38Issue(4)：10-24,15.

中国航空学报（英文版）2025，Vol.38Issue(4)：10-24,15.DOI:10.1016/j.cja.2024.10.007

Pressure oscillation and suppression method of large-aspect-ratio solid rocket motors

Yunzhi XI ¹Jingwei GAO ¹Zeping WU ¹Bolun ZHANG ¹Lijun YANG ¹Jun XIA¹

作者信息

1. College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
折叠

摘要

关键词

Pressure oscillation/Suppression method/Solid rocket motor/Large aspect ratio/Large eddy simulation

Key words

Pressure oscillation/Suppression method/Solid rocket motor/Large aspect ratio/Large eddy simulation

引用本文复制引用

Yunzhi XI,Jingwei GAO,Zeping WU,Bolun ZHANG,Lijun YANG,Jun XIA..Pressure oscillation and suppression method of large-aspect-ratio solid rocket motors[J].中国航空学报（英文版）,2025,38(4):10-24,15.

基金项目

This study was supported by the Natural Science Foundation of Hunan Province of China(No.2023JJ40672)and the Inno-vation Science Fund Project of National University of Defense Technology,China(No.ZK2023-039). （No.2023JJ40672）

中国航空学报（英文版）

ISSN：1000-9361

访问量0

下载量0

段落导航