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时间分辨的普通雨燕飞越一系列飞行速度时的涡尾流。

Time-resolved vortex wake of a common swift flying over a range of flight speeds.

机构信息

Department of Theoretical Ecology, Lund University, 223 62 Lund, Sweden.

出版信息

J R Soc Interface. 2011 Jun 6;8(59):807-16. doi: 10.1098/rsif.2010.0533. Epub 2010 Dec 3.

Abstract

The wake of a freely flying common swift (Apus apus L.) is examined in a wind tunnel at three different flight speeds, 5.7, 7.7 and 9.9 m s(-1). The wake of the bird is visualized using high-speed stereo digital particle image velocimetry (DPIV). Wake images are recorded in the transverse plane, perpendicular to the airflow. The wake of a swift has been studied previously using DPIV and recording wake images in the longitudinal plane, parallel to the airflow. The high-speed DPIV system allows for time-resolved wake sampling and the result shows features that were not discovered in the previous study, but there was approximately a 40 per cent vertical force deficit. As the earlier study also revealed, a pair of wingtip vortices are trailing behind the wingtips, but in addition, a pair of tail vortices and a pair of 'wing root vortices' are found that appear to originate from the wing/body junction. The existence of wing root vortices suggests that the two wings are not acting as a single wing, but are to some extent aerodynamically detached from each other. It is proposed that this is due to the body disrupting the lift distribution over the wing by generating less lift than the wings.

摘要

在三个不同的飞行速度,即 5.7、7.7 和 9.9 m s(-1)下,在风洞中对自由飞行的普通雨燕(Apus apus L.)的尾流进行了检查。使用高速立体数字粒子图像测速法(DPIV)对鸟类的尾流进行了可视化。尾流图像是在横截面上记录的,与气流垂直。先前已经使用 DPIV 对雨燕的尾流进行了研究,并在与气流平行的纵向上记录了尾流图像。高速 DPIV 系统允许对尾流进行时间分辨采样,结果显示出了先前研究中未发现的特征,但垂直力约有 40%的不足。正如早期的研究也揭示的那样,一对翼尖涡尾随在翼尖之后,但此外,还发现了一对尾涡和一对“翼根涡”,它们似乎源自翼/机身的交界处。翼根涡的存在表明,两个机翼并没有作为一个整体机翼发挥作用,而是在某种程度上彼此在气动上分离。据推测,这是由于机身产生的升力小于机翼,从而破坏了机翼上的升力分布。

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