首页> 美国卫生研究院文献>Journal of the Royal Society Interface >Wake structure and wingbeat kinematics of a house-martin Delichon urbica
【2h】

Wake structure and wingbeat kinematics of a house-martin Delichon urbica

机译:马丁·德里奇·乌尔比卡住宅的尾迹结构和脉动运动学

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

The wingbeat kinematics and wake structure of a trained house martin in free, steady flight in a wind tunnel have been studied over a range of flight speeds, and compared and contrasted with similar measurements for a thrush nightingale and a pair of robins. The house martin has a higher aspect ratio (more slender) wing, and is a more obviously agile and aerobatic flyer, catching insects on the wing. The wingbeat is notable for the presence at higher flight speeds of a characteristic pause in the upstroke. The essential characteristics of the wing motions can be reconstructed with a simple two-frequency model derived from Fourier analysis. At slow speeds, the distribution of wake vorticity is more simple than for the other previously measured birds, and the upstroke does not contribute to weight support. The upstroke becomes gradually more significant as the flight speed increases, and although the vortex wake shows a signature of the pause phase, the global circulation measurements are otherwise in good agreement with surprisingly simple aerodynamic models, and with predictions across the different species, implying quite similar aerodynamic performance of the wing sections. The local Reynolds numbers of the wing sections are sufficiently low that the well-known instabilities of attached laminar flows over lifting surfaces, which are known to occur at two to three times this value, may not develop.
机译:在一定的飞行速度范围内,研究了训练有素的马丁在风洞中自由,稳定飞行的机翼运动学和尾流结构,并将其与类似的测量标准进行比较,并与类似的鹅口疮夜莺和一对知更鸟进行了对比。马丁房屋的机翼高(长)长,机翼长得多,并且是一种更明显的敏捷和特技飞行器,在机翼上捕获了昆虫。机翼跳动在较高的飞行速度中会出现特征性的上冲停顿。可以使用从傅立叶分析得出的简单两频模型重建机翼运动的基本特征。在低速下,尾流涡度的分布比之前测得的其他鸟类更简单,并且上冲也无助于支撑体重。随着飞行速度的增加,向上冲程逐渐变得越来越重要,尽管涡流尾迹显示出暂停阶段的特征,但总体而言,全球环流测量值与令人惊讶的简单空气动力学模型以及对不同物种的预测非常吻合,这意味着机翼部分的空气动力学性能相似。机翼部分的局部雷诺数足够低,以至于可能无法形成众所周知的附着在升力面上的层流的不稳定性,众所周知,不稳定性是该值的2至3倍。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号