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Flow diagnosis of compressible vortex structures on a 65° delta-wing

Fanrong XUE Han LIN Shengye WANG Chuanzhen LIU Shufan ZOU Wei LIU

中国航空学报（英文版）2026，Vol.39Issue(3)：47-63,17.

中国航空学报（英文版）2026，Vol.39Issue(3)：47-63,17.DOI:10.1016/j.cja.2025.103942

Flow diagnosis of compressible vortex structures on a 65° delta-wing

Fanrong XUE ¹Han LIN ¹Shengye WANG ¹Chuanzhen LIU ²Shufan ZOU ³Wei LIU¹

作者信息

1. College of Aerospace and Engineering,National University of Defense Technology,Changsha 410073,China
2. China Academy of Aerospace Aerodynamics,Beijing 100071,China
3. College of Aerospace and Engineering,National University of Defense Technology,Changsha 410073,China||State Key Laboratory of High-Efficiency Reusable Aerospace Transportation Technology,Changsha 410073,China
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摘要

关键词

Aerodynamic computed topography/Compressible flow/Delta wing aircraft/Vortex force

Key words

Aerodynamic computed topography/Compressible flow/Delta wing aircraft/Vortex force

引用本文复制引用

Fanrong XUE,Han LIN,Shengye WANG,Chuanzhen LIU,Shufan ZOU,Wei LIU..Flow diagnosis of compressible vortex structures on a 65° delta-wing[J].中国航空学报（英文版）,2026,39(3):47-63,17.

基金项目

The authors gratefully acknowledged the support of the National Natural Science Foundations of China(Nos.12202486,U22B20133,92252101). （Nos.12202486,U22B20133,92252101）

中国航空学报（英文版）

ISSN：1000-9361

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