主动变形扑翼飞行器的设计和风洞试验研究

doi:10.7527/S1000-6893.2013.0083

Abstract

Abstract: The 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, the laws of motion of wing and tail were studied, an active morphing wing ornithopter was designed and built base on robotics. The laws of motion of the ornithopter were presented, a control system was designed and built. Wind tunnel tests of the ornithopter were performed in a low-speed wind tunnel. The lift, thrust characteristics and aerodynamic mechanism were studied, also the influence of wind velocity, flapping frequency, amplitude, stretch phase was investigated. The conventional flapping wing was tested as contrast. The test result shows that the active morphing wing can increase the lift and enhance ability to adapt to flight status.

CLC Number:

V211.7

References

[1] KING, A. S., AND MCLELLAND, J. Form and Func-tion in Birds, 1985, vol. 3. Academic Press, Inc. ISBN 0124075010.
[2] TOBALSKE, B. W., AND DIAL, K. P. Flight kinemat-ics of blackbilled magpies and pigeons over a wide range of speeds. Journal of Experimental Biology, 1996, 199: 263–280.
[3] Bret W. Tobalske. Biomechanics of bird flight. The Journal of Experimental Biology, 2007, 210:3135–3146
[4] Ulla M. Lindhe Norberg, York Winter. Wing beat kine-matics of a nectar-feeding bat, Glossophaga soricina, flying at different flight speeds and Strouhal numbers. The Journal of Experimental Biology, 2006, 209:3887–3897
[5] ANG H S, ZENG R, DUAN W B. Aerodynamic expe-rimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV.Journal of Aerospace Power.2007, 22(11):1938-1845.(in Chinese)
昂海松，曾锐，段文博等.柔性扑翼微型飞行器升力和推力机理的风洞试验和飞行试验.航空动力学报.2007, 22(11):1938-1845
[6] ZHANG Y F，SONG B F，YUAN C S. Lift characte-ristic of the flapping wing micro air Vehicle. Acta Aero-dynamica Sinica, 2008, Vol.26,No.4:519–522. (in Chi-nese)
张亚峰，宋笔峰，袁昌盛等.微型扑翼飞行器升力特性研究.空气动力学学报. 2008, Vol.26, No.4:519–522
[7] Lin C S, Hwu C, Young W B. The thrust and lift of an ornithopter’s membrane wings with simple flapping motion. Aerospace Science and Technology, 2006,10: 111–119
[8] Ramiro Chavez-Alarcon, SHU F J. Lift, Drag and Flow-field Measurements around a Small Ornithopter. Orlando: AIAA, 2011
[9] Billingsley D, Slipher G, Grauer J. Testing of a Passively Morphing Ornithopter Wing. Washington: AIAA, 2009
[10] Mueller D, Gerdes J W, Gupta S K.INCORPORATION OF PASSIVE WING FOLDING IN FLAPPING WING MINIATURE AIR VEHICLES. San Diego: ASME Mechanism and Robotics Conference, 2009
[11] Demetgul M, Pino W, Tansel L N. MORPHING WING DESIGN FOR ORNITHOPTERS. Miami: ECTC, 2008
[12] Li Bing. A Preliminary Study on the Microstructure of Bird Primaries and Their Significance for Flight. Harbin: Northeast Forestry University, 2008.(in Chinese)
李冰.鸟类初级飞羽微观结构与飞行性能相关性的初步研究.哈尔滨：东北林业大学，2008
[13] NORBERG, U. M. Vertebrate Flight. Springer-Verlag. ISBN 0387513701. 1990.
[14] Wu J C, Zoran Popovi′c. Realistic Modeling of Bird Flight Animations. ACM Transactions on Graphics,July 2003,Volume 22 Issue 3:888-895
[15] Pennycuick C. J. Speeds and wingbeat frequencies of migrating birds compared with calculated benchmarks. The Journal of Experimental Biology, 2001, 204:3283–3294
[16] SHAO L M, SONG B F, SONG W P. Experimental research of flapping—wing propulsion for micro air ve-hicles. Journal of Experiments in Fluid Mechanics, 2009, Vol.23,No.1:1–6. (in Chinese)
邵立民，宋笔锋，宋文萍.微型扑翼的推进特性实验研究.实验流体力学. 2009, Vol.23,No.1:1–6.

Design and Wind Tunnel Testing of an Active Morphing Wing Ornithopter

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	WANG Jiming, GAO Yunhai, JIAO Renshan. Numerical simulation of ventral sting interference in high Reynolds number wind tunnel for civil aircraft low speed configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 123526-123526.
[2]	LIU Zhongchen, QIAN Zhansen, LENG Yan, GAO Liangjie. Wind tunnel measurement techniques for sonic boom near-field pressure [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 123596-123596.
[3]	. Unsteady aerodynamics test and modeling of civil transport configuration at extreme flight conditions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[4]	. Multibody Dynamics Analysis of Three-cable Mount System for Full-model Flutter Wind-tunnel Test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[5]	. Review on aircraft-store separation compatibility for the internal weapons [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[6]	JIANG Tao, LI Qiang, CHEN Suyu, CHANG Yu, ZHANG Kouli. Image inpainting of wind tunnel test based on Otsu method and FMM [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 123293-123293.
[7]	ZHANG Junlong, LEI Hongsheng, TIAN Hao, LI Jie. Noise radiation characteristics and source distribution of subsonic rectangular jet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 123386-123386.
[8]	XIE Feng, HONG Guanxin, ZHANG Chenkai, WEI Zhongwu, MA Handong. Ground calibration method of captive trajectory system parallel mechanism [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(1): 423175-423175.
[9]	DU Yufeng, LIN Jun, WANG Xunnian, XIONG Neng. Measurement technique optimization of turbulence level in compressible fluid by changing overheat ratio of hot wire anemometer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 123067-123067.
[10]	LIU Weijie, HE Fan, LING Zhongwei. Predictive active disturbance rejection control for flow field in 2.4 m transonic wind tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 123154-123154.
[11]	. Wind tunnel model flight test technique for advanced fighter aircraft design [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[12]	. Advanced Fighter All-moving V-twin tail Buffet Design, Analysis and Test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[13]	ZHOU Run, ZHANG Zhengyu, YANG Zhenhua, HUANG Xuhui. Single camera videogrammetry measurement method of angle of attack based on homography matrix [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(10): 122800-122800.
[14]	. Experimental Investigations on the Gravity Effects of Light Model Method in the Supersonic Drop-test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[15]	. Unsteady aerodynamic modeling of fighter configuration at high angles of attack [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.