南京航空航天大学学报（英文版）2015，Vol.32Issue(2)：180-186,7.DOI:10.16356/j.1005-1120.2015.02.180
Structural Design and Control of Variable Camber Wing Driven by Ultrasonic Motors
Structural Design and Control of Variable Camber Wing Driven by Ultrasonic Motors
Liu Weidong 1Zhu Hua 1Zhou Shengqiang 1Bai Yalei 1Zhao Chunsheng1
作者信息
- 1. State Key Laboratory of Mechanics and Control of Mechanical Structures ,Nanjing University of Aeronautics and Astronautics ,Nanjing 210016 ,P .R .China
- 折叠
摘要
关键词
variable camber wing/ultrasonic motors(USMs)/morphing skin/control system/wind tunnel testKey words
variable camber wing/ultrasonic motors(USMs)/morphing skin/control system/wind tunnel test分类
航空航天引用本文复制引用
Liu Weidong,Zhu Hua,Zhou Shengqiang,Bai Yalei,Zhao Chunsheng..Structural Design and Control of Variable Camber Wing Driven by Ultrasonic Motors[J].南京航空航天大学学报（英文版）,2015,32(2):180-186,7.
