Thin Film Geometry Design for Flapping Rotor Wing

Jing Lu; Yan Fang Hang; Ying Jun Hu

doi:10.4028/www.scientific.net/AMM.633-634.1299

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 633-634Thin Film Geometry Design for Flapping Rotor Wing

Thin Film Geometry Design for Flapping Rotor Wing

Abstract:

The shape of thin film for flapping rotor wing has a significant impact on aerodynamics. To increase lift, we designed 7 different flexible film wings. Then we compared the aerodynamic force of thin film in accordance with the same aspect ratio of different shapes and the same shape of different aspect ratio. The conclusions suitable for the thin film design guide are obtained. The aspect ratio of thin film for flapping rotor wing is inversely proportional to the aerodynamic force. At the same aspect ratio, the film wing designed by bionic is superior to other shapes. With the aspect ratio increases, the thrust of the film wing designed by bionic decreases faster than the lift.

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Periodical:

Applied Mechanics and Materials (Volumes 633-634)

Pages:

1299-1302

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.633-634.1299

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Online since:

September 2014

Authors:

Jing Lu*, Yan Fang Hang, Ying Jun Hu

Keywords:

Aspect Ratio, Geometry Design, Thin Film

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* - Corresponding Author

References

[1] Shijun Guo, Zhengjie Wang, Ningjun Fan, et al. A kind of flapping and rotor wing micro-miniature air vehicles: China, 200920106095. X[P]. 2009-12-23, ( in Chinese).

Google Scholar

[2] Kim Y J, Choi H C, Kim K H. The comparative study of rigid wing and flexible wing in flapping motion [J]. AIAA 2005-6336, (2005).

DOI: 10.2514/6.2005-6336

Google Scholar

[3] Muniappan A, Baskar V, Duriyanandhan V. Lift and Thrust Characteristics of Flapping Wing Micro Air Vehicle [J]. AIAA 2005-1055, (2005).

DOI: 10.2514/6.2005-1055

Google Scholar

[4] I. E. Garrick, Propulsion of a flapping and oscillating airfoil, naca-report-567(1937)2-3.

Google Scholar

[5] Ellington CP, The novel aerodynamics of insect flight: Applications to micro-air vehicles[J]. The Journal of Experimental Biology, 1999, 202: 3439-3448.

DOI: 10.1242/jeb.202.23.3439

Google Scholar