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Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure changing rate

Bocheng ZHOU Ge WANG Ben GUAN Yan CHEN Zenan YANG

中国航空学报（英文版）2025，Vol.38Issue(5)：37-49,13.

中国航空学报（英文版）2025，Vol.38Issue(5)：37-49,13.DOI:10.1016/j.cja.2024.08.032

Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure changing rate

Bocheng ZHOU ¹Ge WANG ¹Ben GUAN ¹Yan CHEN ¹Zenan YANG¹

作者信息

1. College of Aerospace and Civil Engineering,Harbin Engineering University,Harbin 150001,China
折叠

摘要

关键词

Expansion-deflection nozzle/Shock waves/Self-excited oscillation/Thrust oscillation/Mode transition

Key words

Expansion-deflection nozzle/Shock waves/Self-excited oscillation/Thrust oscillation/Mode transition

引用本文复制引用

Bocheng ZHOU,Ge WANG,Ben GUAN,Yan CHEN,Zenan YANG..Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure changing rate[J].中国航空学报（英文版）,2025,38(5):37-49,13.

基金项目

This work was supported by the National Natural Science Foundation of China(No.12002102). （No.12002102）

中国航空学报（英文版）

ISSN：1000-9361

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