Graduate School of Engineering, Chiba University, 1-33 Yayoi-cho, Inage-ku, Chiba 263-8522, Japan.
Proc Biol Sci. 2012 Feb 22;279(1729):722-31. doi: 10.1098/rspb.2011.1023. Epub 2011 Aug 10.
Insect wings are deformable structures that change shape passively and dynamically owing to inertial and aerodynamic forces during flight. It is still unclear how the three-dimensional and passive change of wing kinematics owing to inherent wing flexibility contributes to unsteady aerodynamics and energetics in insect flapping flight. Here, we perform a systematic fluid-structure interaction based analysis on the aerodynamic performance of a hovering hawkmoth, Manduca, with an integrated computational model of a hovering insect with rigid and flexible wings. Aerodynamic performance of flapping wings with passive deformation or prescribed deformation is evaluated in terms of aerodynamic force, power and efficiency. Our results reveal that wing flexibility can increase downwash in wake and hence aerodynamic force: first, a dynamic wing bending is observed, which delays the breakdown of leading edge vortex near the wing tip, responsible for augmenting the aerodynamic force-production; second, a combination of the dynamic change of wing bending and twist favourably modifies the wing kinematics in the distal area, which leads to the aerodynamic force enhancement immediately before stroke reversal. Moreover, an increase in hovering efficiency of the flexible wing is achieved as a result of the wing twist. An extensive study of wing stiffness effect on aerodynamic performance is further conducted through a tuning of Young's modulus and thickness, indicating that insect wing structures may be optimized not only in terms of aerodynamic performance but also dependent on many factors, such as the wing strength, the circulation capability of wing veins and the control of wing movements.
昆虫翅膀是可变形结构,在飞行过程中会由于惯性和空气动力而被动和动态地改变形状。目前尚不清楚由于固有翼的柔韧性导致的翼运动学的三维和被动变化如何有助于昆虫扑翼飞行中的非定常空气动力学和能量学。在这里,我们对悬停天蛾 Manduca 的空气动力学性能进行了基于流固相互作用的系统分析,采用了具有刚性和柔性翅膀的悬停昆虫综合计算模型。通过对具有被动变形或规定变形的扑翼的空气动力学性能进行评估,得出了空气动力、功率和效率等方面的结果。我们的研究结果表明,翼的柔韧性可以增加尾迹中的下洗,从而增加空气动力:首先,观察到了动态的翼弯曲,这延迟了翼尖附近前缘涡的破裂,从而增强了空气动力的产生;其次,翼弯曲和扭转的动态变化组合有利地改变了翼的远侧区域的运动学,这导致在划桨反转之前立即增强了空气动力。此外,柔性翼的悬停效率也因翼的扭转而提高。通过调整杨氏模量和厚度,进一步研究了翼刚度对空气动力学性能的影响,表明昆虫翼结构不仅可以优化空气动力学性能,还可以依赖于许多因素,如翼的强度、翼脉的环流能力和翼运动的控制。