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多段柔性变体扑翼飞行器设计
引用本文:黄鸣阳,肖天航,昂海松.多段柔性变体扑翼飞行器设计[J].航空动力学报,2016,31(8):1838-1844.
作者姓名:黄鸣阳  肖天航  昂海松
作者单位:南京航空航天大学航空宇航学院飞行器先进设计技术国防重点学科实验室, 南京 210016
基金项目:国家级大学生创新训练计划项目(201310287001);预研项目;江苏高校优势学科建设工程基金资助
摘    要:多段柔性变体扑翼模仿海鸥翅膀的复杂运动.观察海鸥翅膀的运动周期,设计了包含慢频率扑动、展向折弯、弦向扭转和结构柔性变形的扑翼模型,并应用准定常方法计算气动力,为该扑翼飞行器设计提供依据.在CATIA和3DMAX中设计多段柔性变体扑翼机的三维模型和运动模拟,制作样机进行飞行试验,研究其平飞、爬升、偏航等飞行姿态,结果表明升力和推力与数值计算结果吻合.相较于原有扑翼飞行器,多段柔性变体扑翼飞行器可以慢频率扑动飞行,调整扑翼形状. 

关 键 词:多段柔性变体扑翼    扑翼模型    准定常计算方法    运动模拟    飞行试验
收稿时间:2014/11/26 0:00:00

Design of an ornithopter with multisection flexible morphing wings
HUANG Ming-yang,XIAO Tian-hang and ANG Hai-song.Design of an ornithopter with multisection flexible morphing wings[J].Journal of Aerospace Power,2016,31(8):1838-1844.
Authors:HUANG Ming-yang  XIAO Tian-hang and ANG Hai-song
Institution:Ministerial Key Discipline Laboratory of Advanced Design Technology of Aircraft, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The multisection flexible morphing wings mimic the complex movement of seagull''s flapping wings. By observing movement periods of seagull''s flapping wings, a new flapping-wing model including fold, torsion, flexible morphing and slowly beating up and down was built. In order to provide the design of this ornithopter with a theoretical basis, the quasi-steady method was applied to calculate aerodynamic force. The three-dimensional model and motion simulation were built in CATIA and 3DMAX, and an ornithopter with multisection flexible morphing wing was built for flight test. Flying attitudes including level flight,climbing and yawing were studied, and test results including lift and thrust agree with the calculation. Compared with conventional ornithopters, the ornithopter with multisection flexible morphing wing can fly while flapping with a low frequency, and adjusting the shape of flapping wings.
Keywords:multisection flexible morphing wing  flapping-wing model  quasi-steady method  motion simulation  flight test
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