首页|期刊导航|中国航空学报（英文版）|Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning rates

Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning rates

Wen JI Chunlin GONG Chunna LI Gang WANG

中国航空学报（英文版）2026，Vol.39Issue(8)：125-140,16.

中国航空学报（英文版）2026，Vol.39Issue(8)：125-140,16.DOI:10.1016/j.cja.2025.103988

Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning rates

Wen JI ¹Chunlin GONG ¹Chunna LI ¹Gang WANG²

作者信息

1. School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China||Shaanxi Aerospace Flight Vehicle Design Key Laboratory,Xi'an 710072,China
2. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China
折叠

摘要

关键词

Angular motion/Coupled computational fluid dynamics and rigid body dynamics/Dual-spin projectile/Numerical simulation/Unsteady aerodynamic characteristic

Key words

Angular motion/Coupled computational fluid dynamics and rigid body dynamics/Dual-spin projectile/Numerical simulation/Unsteady aerodynamic characteristic

引用本文复制引用

Wen JI,Chunlin GONG,Chunna LI,Gang WANG..Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning rates[J].中国航空学报（英文版）,2026,39(8):125-140,16.

基金项目

This research was supported by the National Natural Science Foundation of China(No.U2141254). （No.U2141254）

中国航空学报（英文版）

ISSN：1000-9361

访问量0

下载量0

段落导航