Effect of bendable wing tip on aerodynamic characteristics of flying-wing configuration aircraft

被引：0
|
作者：
Liu, Zhitao [1 ,2 ]
Jiang, Yong [2 ]
Nie, Bowen [2 ,3 ]
Cen, Fei [2 ]
Xu, Sheng [2 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
[2] Low Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang,621000, China
[3] College of Intelligence Science and Technology, National University of Defense Technology, Changsha,410073, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 06期
关键词：
D O I：
10.7527/S1000-6893.2020.24179
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学科分类号：
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