Improved aerodynamic model for efficient analysis of flapping-wing flight

AIAA Journal

Volumn 49, Issue 4, 2011, Pages 868-872

  Kim, Dae Kwan ^a   Lee, Jun Seong ^b,c   Han, Jae Hung ^b,d  

^a Korea Aerospace Research Institute (KARI)   (South Korea)

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^c Satellite Control System Department   (South Korea)

^d Department of Aerospace Engineering ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 79953134739     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050556     Document Type: Article

References (12)

1. Deng, X., Schenato, L., Wu, W., and Sastry, S., "Flapping Flight for Biomimetic Robotic Insects: Part 1, System Modeling, " IEEE Transactions on Robotics and Automation, Vol.22, No. 4, 2006, pp. 776-788. doi:10.1109/TRO.2006. 875480 (Pubitemid 44263864)
2. Dickson, W. B., Straw, A. D., and Dickinson, M. H., "Integrative Model of Drosophila Flight, " AIAA Journal, Vol. 46, No.9, 2008, pp.2150-2164. doi:10.2514/1.29862
3. Dietl, J. M., and Garcia, E., "Stability in Ornithopter Longitudinal Flight Dynamics, " Journal of Guidance, Control, and Dynamics, Vol. 31, No. 4, 2008, pp.1157-1162. doi:10.2514/1. 33561
4. Grauer, J. A., and Hubbard, J. E., "Multibody Model of An Ornithotper, " Journal of Guidance, Control, and Dynamics, Vol. 32, No. 5, 2009, pp.1675-1679. doi:10.2514/1. 43177
5. Chung, S. -J., and Dorothy, M., "Neurobiologically Inspired Control of Engineered Flapping Flight, " Journal of Guidance, Control, and Dynamics, Vol. 33, No.2, 2010, pp. 440-453. doi:10.2514/1. 45311
6. DeLaurier, J. D., "An Aerodynamic Model for Flapping-Wing Flight, " The Aeronautical Journal, Vol.97, No.964, April 1993, pp.125-130.
7. Liu, H. T., "Unsteady Aerodynamics of a Wortmann Wing at Low Reynolds Numbers, " Journal of Aircraft, Vol.29, No. 4, 1992, pp. 532-539. doi:10.2514/3. 46198
8. Prouty, R. W., Helicopter Performance, Stability, and Control, PWS Engineering, Boston, 1986, Chap. 6.
9. Scherer, J. O., Experimental and Theoretical Investigation of Large Amplitude Oscillating Foil Propulsion Systems, Hydronautics, Laurel, MD, 1968, pp.13-14.
10. Larijani, R. F., and DeLaurier, J. D., "A Nonlinear Aeroelastic Model for the Study of Flapping Wing Flight, " Progress in Astronautics and Aeronautics, Vol.195, AIAA, Reston, VA, 2001, pp. 399-428.
11. Kim, D. -K., Han, J. -H., and Kwon, K. -J., "Wind Tunnel Tests for a Flapping Wing Model with a Changeable Camber Using Macro-Fiber Composite Actuators, " Smart Materials and Structures, Vol.18, No.2, 2009, Paper 024008. doi:10.1088/0964-1726/18/2/024008
12. Okamoto, M., and Azuma, A., "Experimental Study on Aerodynamic Characteristics of Unsteady Wings at Low Reynolds Number, " AIAA Journal, Vol. 43, No.12, 2005, pp.2526-2536. doi:10.2514/1.14813 (Pubitemid 43017396)