主动变形扑翼飞行器的设计和风洞测力试验研究
收稿日期: 2012-03-20
修回日期: 2012-12-07
网络出版日期: 2013-03-29
基金资助
国家自然科学基金(11002072);高等学校博士学科点专项科研基金(20103218120001)
Design and Wind Tunnel Test of an Active Morphing Wing Ornithopter
Received date: 2012-03-20
Revised date: 2012-12-07
Online published: 2013-03-29
Supported by
National Natural Science Foundation of China (11002072);Specialized Research Fund for the Doctoral Program of Higher Education (20103218120001)
段文博 , 昂海松 , 肖天航 . 主动变形扑翼飞行器的设计和风洞测力试验研究[J]. 航空学报, 2013 , 34(3) : 474 -486 . DOI: 10.7527/S1000-6893.2013.0083
An active morphing flapping wing can mimic the complex movement of a flying bird's wings. In order to understand the aerodynamics of the active morphing wing ornithopter, the bird's bone structure as well as the laws of motion of its wing and tail are studied, and an active morphing wing ornithopter is designed and built based on robotics. The laws of motion of the ornithopter are presented, a control system is designed and built. Wind tunnel tests of the ornithopter are performed in a low-speed wind tunnel. The lift and thrust characteristics are studied. Furthermore, the influence of wind velocity, flapping frequency, amplitude and stretch phase on lift and thrust is investigated. A conventional flapping wing is tested for contrast. The test result shows that the active morphing wing can significantly increase the lift and enhance the ability of the ornithopter to adapt to various flight statuses.
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