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蝙蝠进行转弯上升机动的运动学和空气动力学分析。

Kinematic and aerodynamic analysis of a bat performing a turning-ascending maneuver.

机构信息

Department of Mechanical Engineering, Virginia Tech, Blacksburg, VA, United States of America.

出版信息

Bioinspir Biomim. 2021 Feb 13;16(1):016019. doi: 10.1088/1748-3190/abb78d.

DOI:10.1088/1748-3190/abb78d
PMID:33586665
Abstract

The flapping flight of many bat species is characterized by a high degree of maneuverability and provides fertile ground for biomimetic design. However, there has been little prior work toward understanding bat flight maneuvers, particularly using a coupled kinematic and aerodynamic framework. Here, wing kinematic data of a large insectivorous bat (Hipposideros armiger) in straight and turning flight is investigated. Fundamental to turning flight are asymmetries in the wing kinematics and consequently asymmetries in the aerodynamic forces. Forces were calculated from the wing kinematics using aerodynamic numerical simulations. Aspects of the wing kinematics in the turn that were distinguishable from straight flight were an increase in stroke plane deviation angle, nominal increase in flapping amplitude, and a decrease in the horizontal stroke plane angle of the wing inside the turn. While prior work on the mechanics of turning flight in animals has focused on classifying a turn as either banking or yawing, in the present work we show evidence of simultaneous and synergistic banking and yawing mechanisms. During the initiation of the turn, the bank angle was low, and elevated thrust by the outside wing generated a significant yaw rotational moment during both the upstroke and downstroke. Later in the turn, the bank angle increased to approximately 25 degrees tilting the net force vector toward the inside of the turn providing centripetal acceleration thereby turning the bat. Understanding the details of the turning mechanism-combined yaw and bank-provides useful design and control principles for biomimetic flapping MAVs.

摘要

许多蝙蝠物种的拍动飞行具有高度的机动性,为仿生设计提供了肥沃的土壤。然而,对于理解蝙蝠的飞行机动,特别是使用耦合运动学和空气动力学框架来理解蝙蝠的飞行机动,之前的研究工作很少。在这里,研究了直飞和转弯飞行中大型食虫蝙蝠(马来大狐蝠)的翅膀运动学数据。转弯飞行的基本原理是翅膀运动学的不对称性,因此空气动力也不对称。通过空气动力学数值模拟从翅膀运动学计算得到了力。转弯时与直线飞行有区别的翅膀运动学方面包括:冲程平面偏转角增加,标称拍动幅度增加,以及转弯时翅膀水平冲程平面角度减小。尽管先前关于动物转弯飞行力学的研究主要集中在将转弯分类为倾斜转弯或偏航转弯,但在本工作中,我们展示了同时存在倾斜转弯和偏航转弯协同机制的证据。在转弯开始时,倾斜角度较低,外侧翅膀产生的高升力在上下冲程中都会产生显著的偏航旋转力矩。在转弯的后期,倾斜角度增加到大约 25 度,使净力矢量倾斜向转弯内侧,提供向心加速度,从而使蝙蝠转弯。了解转弯机制(结合偏航和倾斜)的细节为仿生扑翼 MAV 提供了有用的设计和控制原理。

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