Aerodynamic interaction of bristled wing pairs in fling
Aerodynamic interaction of bristled wing pairs in fling
复制标题
刚毛翼对在飞行中的空气动力相互作用
DOI:
10.1063/5.0036018
复制
发表时间:
2021-03-01
影响因子:
4.6
通讯作者:
Santhanakrishnan, Arvind
中科院分区:
文献类型:
--
作者:
Kasoju, Vishwa T.;Santhanakrishnan, Arvind
Tiny flying insects of body lengths under 2mm use the "clap-and-fling" mechanism with bristled wings for lift augmentation and drag reduction at a chord-based Reynolds number (Re) onO(10 ). We examine the wing-wing interaction of bristled wings in fling at Re = 10 as a function of initial inter-wing spacing (delta) and degree of overlap between rotation and linear translation. A dynamically scaled robotic platform was used to drive physical models of bristled wing pairs with the following kinematics (all angles relative to vertical): (1) rotation about the trailing edge to angle theta (r), (2) linear translation at a fixed angle (theta (t)), and (3) combined rotation and linear translation. The results show that (1) the cycle-averaged drag coefficient decreased with increasing theta (r) and theta (t) and (2) decreasing delta increased the lift coefficient owing to increased asymmetry in the circulation of leading and trailing edge vortices. A new dimensionless index, reverse flow capacity (RFC), was used to quantify the maximum possible ability of a bristled wing to leak the fluid through the bristles. The drag coefficients were larger for smaller delta and theta (r) despite larger RFC, likely due to the blockage of inter-bristle flow by shear layers around the bristles. Smaller delta during early rotation resulted in the formation of strong positive pressure distribution between the wings, resulting in an increased drag force. The positive pressure region weakened with increasing theta (r), which in turn reduced the drag force. Tiny insects have been previously reported to use large rotational angles in fling, and our findings suggest that a plausible reason is to reduce drag forces.