Rosén M, Hedenström A
Department of Animal Ecology, Lund University, Ecology Building, SE-223 62 Lund, Sweden.
J Exp Biol. 2001 Mar;204(Pt 6):1153-66. doi: 10.1242/jeb.204.6.1153.
We examined the gliding flight performance of a jackdaw Corvus monedula in a wind tunnel. The jackdaw was able to glide steadily at speeds between 6 and 11 m s(-1). The bird changed its wingspan and wing area over this speed range, and we measured the so-called glide super-polar, which is the envelope of fixed-wing glide polars over a range of forward speeds and sinking speeds. The glide super-polar was an inverted U-shape with a minimum sinking speed (V(ms)) at 7.4 m s(-1) and a speed for best glide (V(bg)) at 8.3 m s(-)). At the minimum sinking speed, the associated vertical sinking speed was 0.62 m s(-1). The relationship between the ratio of lift to drag (L:D) and airspeed showed an inverted U-shape with a maximum of 12.6 at 8.5 m s(-1). Wingspan decreased linearly with speed over the whole speed range investigated. The tail was spread extensively at low and moderate speeds; at speeds between 6 and 9 m s(-1), the tail area decreased linearly with speed, and at speeds above 9 m s(-1) the tail was fully furled. Reynolds number calculated with the mean chord as the reference length ranged from 38 000 to 76 000 over the speed range 6-11 m s(-1). Comparisons of the jackdaw flight performance were made with existing theory of gliding flight. We also re-analysed data on span ratios with respect to speed in two other bird species previously studied in wind tunnels. These data indicate that an equation for calculating the span ratio, which minimises the sum of induced and profile drag, does not predict the actual span ratios observed in these birds. We derive an alternative equation on the basis of the observed span ratios for calculating wingspan and wing area with respect to forward speed in gliding birds from information about body mass, maximum wingspan, maximum wing area and maximum coefficient of lift. These alternative equations can be used in combination with any model of gliding flight where wing area and wingspan are considered to calculate sinking rate with respect to forward speed.
我们在风洞中研究了寒鸦(Corvus monedula)的滑翔飞行性能。寒鸦能够在6至11米/秒的速度下稳定滑翔。在这个速度范围内,鸟儿会改变其翼展和翼面积,我们测量了所谓的滑翔超极曲线,它是固定翼滑翔极曲线在一系列前进速度和下沉速度范围内的包络线。滑翔超极曲线呈倒U形,在7.4米/秒时下沉速度最小(V(ms)),在8.3米/秒时最佳滑翔速度(V(bg))。在最小下沉速度时,相关的垂直下沉速度为0.62米/秒。升力与阻力之比(L:D)与空速之间的关系呈倒U形,在8.5米/秒时最大值为12.6。在整个研究的速度范围内,翼展随速度呈线性下降。在低速和中速时,尾巴展开得很宽;在6至9米/秒的速度之间,尾巴面积随速度呈线性减小,在9米/秒以上的速度时,尾巴完全收起。以平均弦长作为参考长度计算的雷诺数在6至11米/秒的速度范围内为38000至76000。将寒鸦的飞行性能与现有的滑翔飞行理论进行了比较。我们还重新分析了之前在风洞中研究的另外两种鸟类的翼展比与速度的数据。这些数据表明,一个用于计算翼展比以最小化诱导阻力和型阻之和的方程并不能预测这些鸟类实际观察到的翼展比。我们根据观察到的翼展比推导出一个替代方程,用于根据体重、最大翼展、最大翼面积和最大升力系数等信息,计算滑翔鸟类相对于前进速度的翼展和翼面积。这些替代方程可与任何考虑翼面积和翼展的滑翔飞行模型结合使用,以计算相对于前进速度的下沉率。