Department of Mechanical Engineering, Shanghai Maritime University, Shanghai, 201306, PR China.
School of Science, Harbin Institute of Technology, Shenzhen, 518055, PR China.
Comput Biol Med. 2022 Jun;145:105421. doi: 10.1016/j.compbiomed.2022.105421. Epub 2022 Mar 21.
Insect wings are typically deformed under aerodynamic and inertial forces. Both the forces are related to kinematic and morphology parameters of the wing. However, how the insects utilize complex wing morphologies and kinematics to generate the forces, and what the exact contributions of the two forces in wing deformation are still unclear. In the study, the aerodynamic and inertial forces produced by a dragonfly forewing are compared quantitively. Then the dynamic deformation behaviors are studied with a three-dimensional finite element model. Finally, roles of the two forces in wing deformation are fully discussed. The two forces increase along the wingspan every moment and they reach maximal consistently near the pterostigma. Because of the asymmetry of angle of attack, the maximal resultant aerodynamic force is about 4 times of that in upstroke. By comparison, the normal component of aerodynamic force plays the leading role in downstroke while the inertial force works mainly in tangential in upstroke. The finite element simulation demonstrates the bending and twisting deformation behaviors of the wing considering both flapping and rotation. The average strain energy in one flapping cycle is 1.23×10 mJ under inertial force and 0.43×10 mJ under aerodynamics respectively. In addition, the rapid rotation can enhance inertial deformation by 6 times. As a result, deformation of dragonfly wing is dominated by its own inertia in flight. The deformation mechanism addressed could inspire the design of flexible flapping airfoils in morphology and kinematics.
昆虫的翅膀通常会在空气动力和惯性力的作用下变形。这两种力都与翅膀的运动学和形态参数有关。然而,昆虫如何利用复杂的翅膀形态和运动学来产生这些力,以及这两种力在翅膀变形中的确切贡献是什么,目前仍不清楚。在这项研究中,定量比较了蜻蜓前翅产生的空气动力和惯性力。然后,通过三维有限元模型研究了动态变形行为。最后,充分讨论了这两种力在翅膀变形中的作用。这两种力在每个时刻都沿着翼展增加,并且在翅基附近达到最大值。由于攻角的不对称性,最大的空气动力合力约为上冲程的 4 倍。相比之下,在下降冲程中,空气动力的法向分量起主要作用,而惯性力在上冲程中主要起切向作用。有限元模拟表明,考虑到扑动和旋转,翅膀会产生弯曲和扭转变形。在惯性力作用下,一个扑动周期的平均应变能为 1.23×10-5mJ,在空气动力作用下为 0.43×10-5mJ。此外,快速旋转可以使惯性变形增加 6 倍。因此,蜻蜓翅膀的变形主要由其自身的惯性在飞行中决定。所提出的变形机制可以启发在形态和运动学方面设计灵活的扑动翼型。