Hybrid wing design of icing wind tunnel supercooled large droplet icing test

被引：0
|
作者：
Shu, Jun [1 ]
Xu, Dongguang [1 ]
Han, Zhirong [1 ]
Li, Si [2 ]
Huang, Xiong [1 ,3 ]
机构：
[1] Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China，Ltd., Shanghai,201210, China
[2] AVIC Aerodynamics Research Institute, Shenyang,110034, China
[3] School of Automation, Northwestern Polytechnical University, Xi’an,710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 01期
关键词：
20;
D O I：
10.7527/S1000-6893.2022.27182
中图分类号：
学科分类号：
摘要：
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