Affiliation:
1. Department of Intelligent and Control Systems, Kyushu Institute of Technology, 680-4 Kawazu, Iizuka 8208502, Fukuoka, Japan
Abstract
The flapping wings of insects undergo large deformations caused by aerodynamic forces, resulting in cambering. Insect-mimetic micro wings for flapping-wing nano air vehicles mimic these characteristic deformations. In this study, a 2.5-dimensional insect-mimetic micro wing model for flapping-wing nano air vehicles is proposed to realize this type of wing. The proposed model includes a wing membrane, a leading edge, a center vein, and a root vein, all of which are modeled as shell elements. The proposed wing is a 2.5-dimensional structure and can thus be fabricated using polymer micromachining. We conducted a design window search to demonstrate the capabilities of the wing. The design windows, which are areas of desirable design solutions in the design parameter space, are iteratively searched using nonlinear finite-element analysis under quasi-steady aerodynamic modeling. Here, thickness is selected as a design parameter. The properties of real insects, polymer materials, and fabrication conditions are used to determine the other parameters. A fabricable design solution that generates sufficient camber is found from the design windows.
Funder
Japan Society for the Promotion of Science KAKENHI
Reference40 articles.
1. The Aerodynamics of Hovering Insect Flight. III. Kinematics;Ellington;Philos. Trans. R. Soc. Lond. B,1984
2. Brodsky, A.K. (1994). The Evolution of Insect Flight, Oxford Science Publication.
3. The aerodynamics of insect flight;Sane;J. Exp. Biol.,2003
4. Hilton, T., Martin, C., Tun, R., and Castelli, V. (2012, January 9–12). The DARPA Nano Air Vehicle Program. Proceedings of the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, TN, USA.
5. Some problems of micro air vehicles development;Galinski;Bull. Pol. Acad. Sci. Technical. Sci.,2007
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献