The Test and Analysis of Nano Mechanical Properties for Dragonfly Wing

Chun Xiang Pan; Xiao Yan Qi; Guang Zhao; Xu Zhuo Guo

doi:10.4028/www.scientific.net/AMM.574.271

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 574The Test and Analysis of Nano Mechanical...

The Test and Analysis of Nano Mechanical Properties for Dragonfly Wing

Abstract:

nanomechanical testing system in this paper has been applied to get elastic modulus and hardness of dragonfly wing, and showing their gradient changes along the wing, and also analyzing the mechanical properties in nanodimension. It is significant to make a further research for specific biological functions of dragonfly wing.

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Periodical:

Applied Mechanics and Materials (Volume 574)

Pages:

271-274

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.574.271

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Online since:

July 2014

Authors:

Chun Xiang Pan*, Xiao Yan Qi, Guang Zhao, Xu Zhuo Guo

Keywords:

Dragonfly Wing, Elastic Modulus, Hardness, Nanomechanical Properties

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* - Corresponding Author

References

[1] Shyy W, Lian Y, Tang J, Viieru D, Liu H. Aerodynamics of low Reynolds number flyers [M]. Cambridge University Press, UK, (2008).

DOI: 10.1017/cbo9780511551154

Google Scholar

[2] Zhao Yan-ru. Dragonfly wing structure properties and Nano mechanical behavior and bionic analysis [D]. Jilin University, Changchun, (2007).

Google Scholar

[3] Ahearne M, Yang Y, Then K, Liu K. An Indentation technique to characterize the mechanical and viscoelastic properties of human and porcine corneas [J]. Ann. Biomed. Eng. 2007, 35(9): 1608–1616.

DOI: 10.1007/s10439-007-9323-9

Google Scholar

[4] Li Ming, Wen Shi-tao. Theoretical foundation of Nano indention technology [J]. Journal of Mechanical engineering, 2003, (3): 142-145.

Google Scholar

[5] Pathak S, Swadener J G, Kalidindi S R, et al. Measuring the dynamic mechanical response of hydrated mouse bone by nanoindentation[J]. Journal of the Mechanical Behavior of Biomedical Materials, 2011, 4(1): 34-43.

DOI: 10.1016/j.jmbbm.2010.09.002

Google Scholar

[6] Sun Ji-yu, Tong Jin, Ma Yun-hai, et al. Research on stress exponent for creep of insect cuticle used by nannoindenter[C]/International Conference on Cellular, Molecular Biology, Biophysics and Bioengineering, Lushan, China, 2010: 50-53.

Google Scholar