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鸟类翅膀的空气动力学偏航力矩特性

Aerodynamic yawing moment characteristics of bird wings.

作者信息

Sachs Gottfried

机构信息

Institute of Flight Mechanics and Flight Control, Technische Universität München, Boltzmannstr. 15, 85748 Garching, Germany.

出版信息

J Theor Biol. 2005 Jun 21;234(4):471-8. doi: 10.1016/j.jtbi.2004.12.001.

Abstract

The aerodynamic yawing moments due to sideslip are considered for wings of birds. Reference is made to the experience with aircraft wings in order to identify features which are significant for the yawing moment characteristics. Thus, it can be shown that wing sweep, aspect ratio and lift coefficient have a great impact. Focus of the paper is on wing sweep which can considerably increase the yawing moment due to sideslip when compared with unswept wings. There are many birds the wings of which employ sweep. To show the effect of sweep for birds, the aerodynamic characteristics of a gull wing which is considered as a representative example are treated in detail. For this purpose, a sophisticated aerodynamic method is used to compute results of high precision. The yawing moments of the gull wing with respect to the sideslip angle and the lift coefficient are determined. They show a significant level of yaw stability which strongly increases with the lift coefficient. It is particularly high in the lift coefficient region of best gliding flight conditions. In order to make the effect of sweep more perspicuous, a modification of the gull wing employing no sweep is considered for comparison. It turns out that the unswept wing yields yawing moments which are substantially smaller than those of the original gull wing with sweep. Another feature significant for the yawing moment characteristics concerns the fact that sweep is at the outer part of bird wings. By considering the underlying physical mechanism, it is shown that this feature is most important for the efficiency of wing sweep. To sum up, wing sweep provides a primary contribution to the yawing moments. It may be concluded that this is an essential reason why there is sweep in bird wings.

摘要

对于鸟类的翅膀,考虑了由侧滑引起的气动力偏航力矩。参考飞机机翼的经验,以确定对偏航力矩特性有重要意义的特征。因此,可以看出机翼后掠角、展弦比和升力系数有很大影响。本文的重点是机翼后掠角,与未后掠的机翼相比,它会因侧滑而显著增加偏航力矩。有许多鸟类的翅膀采用了后掠。为了展示后掠对鸟类的影响,详细研究了被视为典型例子的海鸥翅膀的空气动力学特性。为此,使用了一种复杂的空气动力学方法来计算高精度的结果。确定了海鸥翅膀相对于侧滑角和升力系数的偏航力矩。它们显示出显著的偏航稳定性水平,且随着升力系数的增加而强烈增加。在最佳滑翔飞行条件的升力系数区域尤其高。为了使后掠的效果更明显,考虑了一个不采用后掠的海鸥翅膀变体用于比较。结果表明,未后掠的机翼产生的偏航力矩明显小于原始有后掠的海鸥翅膀。对偏航力矩特性另一个重要的特征是后掠位于鸟类翅膀的外部。通过考虑其潜在的物理机制,表明这一特征对机翼后掠的效率最为重要。总之,机翼后掠对偏航力矩有主要贡献。可以得出结论,这是鸟类翅膀存在后掠的一个重要原因。

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