Tucker V A
Department of Biology, Duke University, Box 90338, Durham, NC 27708-0338, USA.
J Exp Biol. 2000 Dec;203(Pt 24):3733-44. doi: 10.1242/jeb.203.24.3733.
Raptors - falcons, hawks and eagles in this study - such as peregrine falcons (Falco peregrinus) that attack distant prey from high-speed dives face a paradox. Anatomical and behavioral measurements show that raptors of many species must turn their heads approximately 40 degrees to one side to see the prey straight ahead with maximum visual acuity, yet turning the head would presumably slow their diving speed by increasing aerodynamic drag. This paper investigates the aerodynamic drag part of this paradox by measuring the drag and torque on wingless model bodies of a peregrine falcon and a red-tailed hawk (Buteo jamaicensis) with straight and turned heads in a wind tunnel at a speed of 11.7 m s(-)(1). With a turned head, drag increased more than 50 %, and torque developed that tended to yaw the model towards the direction in which the head pointed. Mathematical models for the drag required to prevent yawing showed that the total drag could plausibly more than double with head-turning. Thus, the presumption about increased drag in the paradox is correct. The relationships between drag, head angle and torque developed here are prerequisites to the explanation of how a raptor could avoid the paradox by holding its head straight and flying along a spiral path that keeps its line of sight for maximum acuity pointed sideways at the prey. Although the spiral path to the prey is longer than the straight path, the raptor's higher speed can theoretically compensate for the difference in distances; and wild peregrines do indeed approach prey by flying along curved paths that resemble spirals. In addition to providing data that explain the paradox, this paper reports the lowest drag coefficients yet measured for raptor bodies (0.11 for the peregrine and 0.12 for the red-tailed hawk) when the body models with straight heads were set to pitch and yaw angles for minimum drag. These values are markedly lower than value of the parasite drag coefficient (C(D,par)) of 0.18 previously used for calculating the gliding performance of a peregrine. The accuracy with which drag coefficients measured on wingless bird bodies in a wind tunnel represent the C(D,par) of a living bird is unknown. Another method for determining C(D,par) selects values that improve the fit between speeds predicted by mathematical models and those observed in living birds. This method yields lower values for C(D,par) (0.05-0.07) than wind tunnel measurements, and the present study suggests a value of 0.1 for raptors as a compromise.
猛禽——本研究中的隼、鹰和雕——比如从高速俯冲中攻击远处猎物的游隼(Falco peregrinus)面临着一个矛盾。解剖学和行为学测量表明,许多种类的猛禽必须将头部向一侧转动大约40度,才能以最大视力直视前方的猎物,但转动头部可能会因增加空气阻力而降低其俯冲速度。本文通过在风洞中以11.7米/秒的速度测量游隼和赤尾鹰(Buteo jamaicensis)无头和转头的无翼模型身体上的阻力和扭矩,研究了这一矛盾中的空气阻力部分。当头部转动时,阻力增加超过50%,并且产生了使模型朝着头部所指方向偏航的扭矩。防止偏航所需阻力的数学模型表明,随着头部转动,总阻力可能会增加一倍以上。因此,矛盾中关于阻力增加的推测是正确的。这里所揭示的阻力、头部角度和扭矩之间的关系,是解释猛禽如何通过保持头部伸直并沿着螺旋路径飞行来避免这一矛盾的前提条件,这种螺旋路径能使其最大视力的视线侧向指向猎物。虽然飞向猎物的螺旋路径比直线路径更长,但猛禽更高的速度理论上可以弥补距离上的差异;野生游隼确实是沿着类似螺旋的弯曲路径接近猎物的。除了提供解释这一矛盾的数据外,本文还报告了在风洞中当无头身体模型设置为最小阻力的俯仰和偏航角度时,猛禽身体所测得的最低阻力系数(游隼为0.11,赤尾鹰为0.12)。这些值明显低于之前用于计算游隼滑翔性能的寄生阻力系数(C(D,par))值0.18。在风洞中对无翼鸟类身体测量的阻力系数能多准确地代表活鸟的C(D,par)尚不清楚。另一种确定C(D,par)的方法是选择能改善数学模型预测速度与活鸟观察速度之间拟合度的值。这种方法得出的C(D,par)值(0.05 - 0.07)比风洞测量值更低,本研究建议将猛禽的C(D,par)值定为0.1作为折衷。