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Aero-propulsive coupling performance and design of distributed propulsion wing

Kelei WANG Zhou ZHOU

中国航空学报（英文版）2025，Vol.38Issue(4)：127-141,15.

中国航空学报（英文版）2025，Vol.38Issue(4)：127-141,15.DOI:10.1016/j.cja.2024.12.002

Aero-propulsive coupling performance and design of distributed propulsion wing

Kelei WANG ¹Zhou ZHOU¹

作者信息

1. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,China
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摘要

关键词

Distributed propulsion wing/Aero-propulsive coupling performance/Multi-level collaboration optimization design method/Decomposition principle/Thrust-drag balance

Key words

Distributed propulsion wing/Aero-propulsive coupling performance/Multi-level collaboration optimization design method/Decomposition principle/Thrust-drag balance

引用本文复制引用

Kelei WANG,Zhou ZHOU..Aero-propulsive coupling performance and design of distributed propulsion wing[J].中国航空学报（英文版）,2025,38(4):127-141,15.

基金项目

This study was co-supported by the Equipment Advance Research Project of China(No.50911040803),the National Defense Pre-research Foundation of China(No.2021-JCJQ-JJ-0805),and the Aeronautical Science Foundation of China(No.2024Z006053001). （No.50911040803）

中国航空学报（英文版）

ISSN：1000-9361

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