首页> 美国卫生研究院文献>Journal of the Royal Society Interface >Wing tucks are a response to atmospheric turbulence in the soaring flight of the steppe eagle Aquila nipalensis
【2h】

Wing tucks are a response to atmospheric turbulence in the soaring flight of the steppe eagle Aquila nipalensis

机译:翼tu是草原鹰Aquila nipalensis飞翔飞行时对大气湍流的反应

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

Turbulent atmospheric conditions represent a challenge to stable flight in soaring birds, which are often seen to drop their wings in a transient motion that we call a tuck. Here, we investigate the mechanics, occurrence and causation of wing tucking in a captive steppe eagle Aquila nipalensis, using ground-based video and onboard inertial instrumentation. Statistical analysis of 2594 tucks, identified automatically from 45 flights, reveals that wing tucks occur more frequently under conditions of higher atmospheric turbulence. Furthermore, wing tucks are usually preceded by transient increases in airspeed, load factor and pitch rate, consistent with the bird encountering a headwind gust. The tuck itself immediately follows a rapid drop in angle of attack, caused by a downdraft or nose-down pitch motion, which produces a rapid drop in load factor. Positive aerodynamic loading acts to elevate the wings, and the resulting aerodynamic moment must therefore be balanced in soaring by an opposing musculoskeletal moment. Wing tucking presumably occurs when the reduction in the aerodynamic moment caused by a drop in load factor is not met by an equivalent reduction in the applied musculoskeletal moment. We conclude that wing tucks represent a gust response precipitated by a transient drop in aerodynamic loading.
机译:湍流的大气条件对高飞的鸟类稳定飞行提出了挑战,通常可以看到它们以一种称为“ motion”的瞬时运动而使翅膀掉落。在这里,我们使用地面视频和机载惯性仪器,对圈养的草原鹰天鹰座鹰的折皱机理,发生原因进行了调查。对从45个飞行中自动识别出的2594个cks的统计分析表明,在较高的湍流条件下,机翼tu的发生频率更高。此外,机翼通常在空速,负荷系数和俯仰率瞬时增加之前,与鸟类遇到逆风阵风一致。由于向下气流或机头向下俯仰运动而引起的攻角迅速下降,从而引起载荷系数的快速下降,子本身立即随之下降。积极的空气动力作用可以使机翼升起,因此,在产生的空气动力力矩必须通过相对的肌肉骨骼力矩来平衡腾飞。当由载荷系数下降引起的空气动力学力矩的减小不能通过等效的施加的肌肉骨骼力矩的减小来满足时,可能会发生机翼褶皱。我们得出的结论是,翼tu代表了由气动载荷的瞬时下降引起的阵风反应。

著录项

相似文献

  • 外文文献
  • 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