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Feather roughness reduces flow separation during low Reynolds number glides of swifts

机译:在低雷诺数滑移下滑时,羽毛粗糙度会降低流动分离

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摘要

Swifts are aerodynamically sophisticated birds with a small arm and large hand wing that provides them with exquisite control over their glide performance. However, their hand wings have a seemingly unsophisticated surface roughness that is poised to disturb flow. This roughness of about 2% chord length is formed by the valleys and ridges of overlapping primary feathers with thick protruding rachides, which make the wing stiffer. An earlier flow study of laminar–turbulent boundary layer transition over prepared swift wings suggests that swifts can attain laminar flow at low angle-of-attack. In contrast, aerodynamic design theory suggests that airfoils must be extremely smooth to attain such laminar flow. In hummingbirds, which have similarly rough wings, flow measurements on a 3D printed model suggests that the flow separates at the leading edge and becomes turbulent well above the rachis bumps in a detached shear layer. The aerodynamic function of wing roughness in small birds is, therefore, not fully understood. Here we perform particle image velocimetry and force measurements to compare smooth versus rough 3D-printed models of the swift hand wing. The high-resolution boundary layer measurements show that the flow over rough wings is indeed laminar at low angle-of-attack and Reynolds number, but becomes turbulent at higher values. In contrast, the boundary layer over the smooth wing forms open laminar separation bubbles that extend beyond the trailing edge. The boundary layer dynamics of the smooth surface varies nonlinear as a function of angle-of-attack and Reynolds number, whereas the rough surface boasts more consistent turbulent boundary layer dynamics. Comparison of the corresponding drag values, lift values, and glide ratios suggests, however, that glide performance is equivalent. The increased structural performance, boundary layer robustness, and equivalent aerodynamic performance of rough wings might have provided small (proto) birds with an evolutionary window to high glide performance.
机译:雨燕是空气动力学上先进的飞鸟,带有小臂和大手翼,可以为滑翔性能提供出色的控制。但是,它们的手翼表面粗糙度似乎很复杂,势必会干扰流动。弦长约2%的粗糙度是由重叠的主要羽毛的谷和隆脊形成的,这些羽毛具有厚的突出的网纹,使机翼变硬。较早的流动研究表明,在准备好的机翼上进行层流-湍流边界层过渡时,在低攻角下,水流可以达到层流。相反,空气动力学设计理论表明,机翼必须极其光滑才能达到这种层流。在具有类似粗糙翅膀的蜂鸟中,在3D打印模型上进行的流量测量表明,流量在前缘处分离,并在分离的剪切层中的rachi凸起上方变得湍流。因此,尚未完全了解小鸟的机翼粗糙度的空气动力学功能。在这里,我们执行粒子图像测速和力测量,以比较快速手翼的平滑3D打印模型与粗糙3D打印模型。高分辨率边界层的测量结果表明,在低攻角和雷诺数下,粗糙机翼上的气流确实是层流的,但在较高值下却变得湍流。相反,光滑机翼上的边界层形成了开放的层流分离气泡,这些气泡延伸到后缘之外。光滑表面的边界层动力学随攻角和雷诺数的变化而非线性变化,而粗糙表面具有更一致的湍流边界层动力学。比较相应的阻力值,升力值和滑行比,可以认为,滑行性能是等效的。粗糙机翼的增加的结构性能,边界层坚固性和等效的空气动力性能可能为小型(原始)鸟类提供了向高滑翔性能进化的窗口。

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