Propulsion/aerodynamic coupling modeling for distributed-propulsion-wing with induced wing configuration

被引：0
|
作者：
Zhao, Qingfeng [1 ]
Zhou, Zhou [1 ]
Li, Minghao [1 ]
Xu, De [2 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi’an,710072, China
[2] School of Computer Science and Technology, Northwestern Polytechnical University, Xi’an,710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷 / 10期
关键词：
31;
D O I：
10.7527/S1000-6893.2023.29252
中图分类号：
学科分类号：
摘要：
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