Experimental Study on Piezoelectric-Stack-Actuator-Driven Active Vibration Control of Helicopter Floor Structure

被引:9
作者
Meng, De [1 ]
Xia, Pinqi [1 ]
Song, Laishou [1 ]
Smith, Edward C. [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing 210016, Peoples R China
[2] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
来源
JOURNAL OF AIRCRAFT | 2020年 / 57卷 / 02期
基金
中国国家自然科学基金;
关键词
D O I
10.2514/1.C035607
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:377 / 382
页数:6
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