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A simulation-based study on longitudinal gust response of flexible flapping wings

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Abstract

Winged animals such as insects are capable of flying and surviving in an unsteady and unpredictable aerial environment. They generate and control aerodynamic forces by flapping their flexible wings. While the dynamic shape changes of their flapping wings are known to enhance the efficiency of their flight, they can also affect the stability of a flapping wing flyer under unpredictable disturbances by responding to the sudden changes of aerodynamic forces on the wing. In order to test the hypothesis, the gust response of flexible flapping wings is investigated numerically with a specific focus on the passive maintenance of aerodynamic forces by the wing flexibility. The computational model is based on a dynamic flight simulator that can incorporate the realistic morphology, the kinematics, the structural dynamics, the aerodynamics and the fluid–structure interactions of a hovering hawkmoth. The longitudinal gusts are imposed against the tethered model of a hovering hawkmoth with flexible flapping wings. It is found that the aerodynamic forces on the flapping wings are affected by the gust, because of the increase or decrease in relative wingtip velocity or kinematic angle of attack. The passive shape change of flexible wings can, however, reduce the changes in the magnitude and direction of aerodynamic forces by the gusts from various directions, except for the downward gust. Such adaptive response of the flexible structure to stabilise the attitude can be classified into the mechanical feedback, which works passively with minimal delay, and is of great importance to the design of bio-inspired flapping wings for micro-air vehicles.

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Acknowledgements

This work was partly supported by the Grant-in-Aid for Scientific Research on Innovative Areas, the Japan Society for the Promotion of Science (Grant 24120007), and the Japan Society for the Promotion of Science KAKENHI (Grant JP17K17638).

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Authors and Affiliations

  1. Graduate School of Engineering, Chiba University, Chiba, 263-8522, Japan

    Toshiyuki Nakata, Shinobu Kumagai & Hao Liu

  2. Department of Mechanical Engineering, Kanto Gakuin University, Kanagawa, 263-8501, Japan

    Ryusuke Noda

Authors
  1. Toshiyuki Nakata
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  2. Ryusuke Noda
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  3. Shinobu Kumagai
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  4. Hao Liu
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Correspondence to Toshiyuki Nakata or Hao Liu.

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Nakata, T., Noda, R., Kumagai, S. et al. A simulation-based study on longitudinal gust response of flexible flapping wings. Acta Mech. Sin. 34, 1048–1060 (2018). https://doi.org/10.1007/s10409-018-0789-5

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  • DOI: https://doi.org/10.1007/s10409-018-0789-5

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