Rotor blade-vortex interaction noise location and surface pressure in skew descending flight

被引：0
|
作者：
Liu, Zhengjiang [1 ]
Wang, Wentao [1 ]
Lin, Yongfeng [1 ]
Cao, Yaxiong [1 ]
机构：
[1] Key Laboratory, China Helicopter Research and Development Institute, Jingdezhen,333000, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2020年 / 41卷 / 12期
关键词：
26;
D O I：
10.7527/S1000-6893.2020.24060
中图分类号：
学科分类号：
摘要：
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