Aerodynamics of an adaptive wing for MAVs

被引：0

作者：

Liu, Xuan ^{[1
,2
]}

Zhu, Rong ^{[1
]}

Liu, Jingwei ^{[1
]}

Zhou, Zhaoying ^{[1
]}

Ye, Xiongying ^{[1
]}

机构：

[1] State Key Laboratory of Precision Measurement Technology and Instruments, Department of Precision Instruments and Mechanology, Tsinghua University, Beijing 100084, China

[2] Institute of Aviation Equipment, Naval Academy of Armament, Shanghai 200436, China

来源：

Qinghua Daxue Xuebao/Journal of Tsinghua University | 2008年 / 48卷 / 05期

关键词：

Adaptive wing - Aerodynamic efficiency - Angles of attack - Driving device - High-efficiency - Low Reynolds number - Particle imaging velocimetry - Wind tunnel tests;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：789 / 791