The Sensitivity of Aerodynamic Forces to Multi-parameters in a Bird-like Flapping Wing

Authors

  • Changtao Ding Zhejiang Industry Polytechnic College, No.151 Qutun Road, Shaoxing 312000,
  • Yuanjun Lv Zhejiang Industry Polytechnic College, No.151 Qutun Road, Shaoxing 312000,
  • Min Lu Zhejiang Industry Polytechnic College, No.151 Qutun Road, Shaoxing 312000,

DOI:

https://doi.org/10.5614/j.eng.technol.sci.2018.50.5.5

Keywords:

aerodynamic forces, bird-like flapping wing, flapping frequency, multi-parameters, Taguchi orthogonal method.

Abstract

The sensitivity of aerodynamic forces in a bird-like flapping wing was numerically studied by analyzing the aerodynamic force states under different parameters. First, the physical model and the kinematic model of the bird-like flapping wing were separately established. Then the aerodynamic force model was established and some important parameters were analyzed by adopting the Taguchi orthogonal method. Finally, a simulation was carried out, from which the order of the parameters was separately determined according to the parameters' effect on lift or thrust. The results showed that increasing the flapping frequency is one of the most important ways to increase lift and thrust. The lift can be increased by increasing the flight velocity, while the thrust can be increased by increasing the maximum flapping angle. The lift or the thrust becomes larger when the incidence angle is approximately or .

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References

Toshiyuki, N., Liu, H. & Bomphrey, R. J., A CFD-informed Quasi-steady Model of Flapping Wing Aerodynamics, Journal of Fluid Mechanics, 783, pp. 323-343, 2015.

Stewart, E., Patil, M., Canfield, R. & Snyder, R.D., Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles, International Journal of Micro Air Vehicles, 4(4), pp. 179-202, 2013.

Phan, H.V., Truong, Q.T., Au, T.K. & Park, H.C., Optimal Flapping Wing for Maximum Vertical Aerodynamic Force in Hover: Twisted or Flat?, Bioinspiration & Biomimetics, 11(4), pp. 046007, 2016.

Sujoy, M. & Ranjan, G., Nonlinear Dynamic Analysis of Dragonfly-inspired Piezoelectric Unimorph Actuated Flapping and Twisting Wing, International Journal of Smart & Nano Materials, 3(2), pp. 103-122, 2012.

Truong, Q.T., Nguyen, Q.V., Truong, V.T., Park, H.C., Byun, D.Y. & Goo, N.S., Estimation of Force Generated by a Beetle-mimicking Flapping Wing System by Using the Blade Element Theory, Proceedings of SPIE - The International Society for Optical Engineering, 79750M-79750M-11, 2011.

Yang, Y. & Xie, Y., Aerodynamic Force Analysis on Wing of Bionic flapping wing Robot Based on Fluent, Machine Tool & Hydraulics, 43(15), pp. 163-165, 193, Aug. 2015.

Yang, W.Q., Song, B.F., Song, W.P., Wang, L.G., Fu, P. & Xu, J.H., Aerodynamic Research of Flexible Flapping Wing by Combining DIC and CFD Approaches, 29th Congress of the International Council of the Aeronautical Sciences, pp. 1-7, Sep. 2014.

Vinh, N.D., Dynamics and Control of a Flapping Wing Aircraft, Masters, Ho Chi Minh University of Technology, 2006.

Zhang, X.J. & Hu, S.L., Influence of Wing Shape on the Aerodynamic Characteristics of Flapping Wing Vehicle, Flight Dynamics, 33(1), pp. 18-20,25, Feb. 2015.

Yang, W.Q., Song, B.F., Song, W.P. & Wang, L.G., The Effects of Span-wise and Chord-wise Flexibility on the Aerodynamic Performance of Micro Flapping Wing, Chinese Science Bulletin, 57(22), pp. 2887-2897, 2012.

Lua, K.B., Lim, T.T. & Yeo, K.S., Effect of Wing-wake Interaction on Aerodynamic Force Generation on a 2D Flapping Wing, Experiments in Fluids, 51(1), pp. 177-195, 2011.

Banerjee, A., Ghosh, S.K. & Das, D., Aerodynamics of Flapping Wing at Low Reynolds Numbers: Force Measurement and Flow Visualization, Isrn Mechanical Engineering, 2011(23), 2014.

Zhu, J. & Lei, B., Effect of a Flapping Wing Geometry on its Aerodynamic Performance, International Conference on Robotics and Automation Engineering, pp.44-47, 2016.

https://www.vcg.com/creative/809720339, retrieved 15 October, 2017.

https://www.duitang.com/blog/?id=453389632, retrieved 15 October, 2017.

http://www.photophoto.cn/show/14202187.html, retrieved 15 October, 2017.

http://www.quanjing.com/imgbuy/ibxmcs04001411.html, retrieved 15 October, 2017.

http://blog.sina.com.cn/s/blog_485b09aa0102vkca.html,15 October, 2017.

https://baike.baidu.com/pic/%E4%BF%A1%E5%A4%A9%E7%BF%81/454705/21191299/6c63514a83a7c41009f7ef1c?fr=lemma&ct=cover#aid=207253&pic=11385343fbf2b211ae7e97bcca8065380dd78eeb, retrieved 15 October, 2017.

Ou, K., Castonguay, P. & Jameson, A., 3D Flapping Wing Simulation with High Order Spectral Difference Method on Deformable Mesh, 49th AIAA Aerospace Sciences Meeting, pp.1-17, Jan. 2011.

Djojodihardjo, H., Ramli, A. S. S. & Wiriadidjaja, S., Kinematic and Aerodynamic Modelling of Flapping Wing Ornithopter, Procedia Engineering, 50(9), pp. 848-863, 2012.

Coclici, C.A. & Wendland, W.L., On the Treatment of the Kutta-Joukowski Condition in Transonic Flow Computations, Journal of Applied Mathematics and Mechanics, 79(8), pp. 507-534, 2015.

Taguchi, G., Systems of Experimental Design: Engineering Methods to Optimize Quality and Minimize Costs, UNIPUBa, Kraus International Publications, 1987.

Durrani, N., Zaheer, S. & Qin, N., Delaunay Graph Mapping-Based Mesh Deformation for Simulation of a Spanwise Rigid and Flexible Flapping NACA0012 Wing Using DES with Parallel Implementation, Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, pp. 1-14, 2011.

Arabagi, V., Hines, L. & Sitti, M., A Simulation and Design Tool for a Passive Rotation Flapping Wing Mechanism, ASME Transactions on Mechatronics, 18(2), pp. 787-798, 2013.

Djojodihardjo, H. & Ramli, A. S. S., Modeling Studies of Bi- and Quad-Wing Flapping Ornithopter Kinematics and Aerodynamics, International Journal of Automotive & Mechanical Engineering, 9/4?pp. 2180-1606, 2014.

Yu, C.J. & Yan, H., Aerodynamic Computation of Flapping-Wing Simulating Pigeon, Journal of Nanchang Hangkong University, 22(2), pp. 39-43, 2008.

Hu, Y.Q., Some Dynamic Problems in Micro Air Vehicles, Doctor Thesis of Nanjing University of Aeronautics and Astronautics, 2002.

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Published

2018-11-30

How to Cite

Ding, C., Lv, Y., & Lu, M. (2018). The Sensitivity of Aerodynamic Forces to Multi-parameters in a Bird-like Flapping Wing. Journal of Engineering and Technological Sciences, 50(5), 650-669. https://doi.org/10.5614/j.eng.technol.sci.2018.50.5.5

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