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关于尾部在鸟类拍翼飞行的稳定性和能量消耗中的作用。

On the role of tail in stability and energetic cost of bird flapping flight.

机构信息

Institute of Mechanics, Materials, and Civil Engineering, UCLouvain, 1348, Louvain-la-Neuve, Belgium.

(DICATECh) Dipartimento di Ingegneria Civile, Ambientale, del Territorio, Edile e di Chimica, Politecnico di Bari, Via Re David 200, 70126, Bari, Italy.

出版信息

Sci Rep. 2022 Dec 31;12(1):22629. doi: 10.1038/s41598-022-27179-7.

Abstract

Migratory birds travel over impressively long distances. Consequently, they have to adopt flight regimes being both efficient-in order to spare their metabolic resources-and robust to perturbations. This paper investigates the relationship between both aspects, i.e., energetic performance and stability, in flapping flight of migratory birds. Relying on a poly-articulated wing morphing model and a tail-like surface, several families of steady flight regime have been identified and analysed. These families differ by their wing kinematics and tail opening. A systematic parametric search analysis has been carried out, in order to evaluate power consumption and cost of transport. A framework tailored for assessing limit cycles, namely Floquet theory, is used to numerically study flight stability. Our results show that under certain conditions, an inherent passive stability of steady and level flight can be achieved. In particular, we find that progressively opening the tail leads to passively stable flight regimes. Within these passively stable regimes, the tail can produce either upward or downward lift. However, these configurations entail an increase of cost of transport at high velocities penalizing fast forward flight regimes. Our model-based predictions suggest that long range flights require a furled tail configuration, as confirmed by field observations, and consequently need to rely on alternative mechanisms to stabilize the flight.

摘要

候鸟的迁徙距离非常遥远。因此,它们必须采用既高效(以节省代谢资源)又稳健(免受干扰)的飞行模式。本文研究了候鸟拍动飞行中能量性能和稳定性之间的关系。通过使用多关节翼型变形模型和类似尾巴的表面,确定并分析了几种稳定的飞行模式。这些模式的区别在于其翅膀的运动学和尾巴的张开角度。进行了系统的参数搜索分析,以评估功耗和运输成本。我们使用专门用于评估极限环的 Floquet 理论框架,通过数值研究来研究飞行稳定性。研究结果表明,在某些条件下,可以实现稳定水平飞行的固有被动稳定性。特别是,我们发现逐渐打开尾巴可以产生被动稳定的飞行模式。在这些被动稳定的模式中,尾巴可以产生向上或向下的升力。然而,这些配置在高速时会导致运输成本增加,从而不利于快速前向飞行模式。我们的基于模型的预测表明,长距离飞行需要收起尾巴的配置,这与实地观察结果一致,因此需要依靠其他机制来稳定飞行。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ed33/9805461/7106f262ad32/41598_2022_27179_Fig1_HTML.jpg

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